rocket_heatfeb15

toc

Table of contents <a href= general geometry Grap ... ee boundary layer Cold forced boundary layer Three calculations of total heat (check these) 1 2 3 " width="618" height="964" align="absmiddle" />

TODO
add nozzles
  thermo weight numberof nozzles
calculate minium thickness for
    between tubes, for strength
    thickness in nozzle
    chamber thickness
number of inner tubes modulo number of nozzles
add additiona partial tubes
calculate temperature of chamber surface and tubes
or calculate thickness as a temperature requierment
seperate materials for inner and outer
:

Rocket engine calculations

RowBox[{RowBox[{(*, 6894.8, *)}], , RowBox[{RowBox[{RowBox[{metertoinch, , =, , 39.3 ... ;local.004365, ,, thermalConductivity.21}], }}]}], ;}], , , }]}]

RowBox[{RowBox[{If, [, RowBox[{False, ,, (* 420m/s 5000psi case *), , RowBox[{TChamber ... #961;local, ;}], , (* density at freestream *), , ,}], ]}], ;}], , }] Null

general

General

A rotary rocket pumps its fuel by rotating, and the centrifugal effects pump the fuel.  The design I'll describe here is ultra simple.  Its design optimizes for simplicity and manufacturability, and incidentally has very high Thrust/Weight as a result of that simplicity.  Some of the design choices drive the design, in particular the choice of fuels, LOX and liquid propane.  Since both are liquid at 90K the require no insulation in the engine or tankage  We start with the assumption of  600m/s rotational velocity and a combustion chamber pressure of 10,000 psi, we may adjust those upwards later.

The engine is made out of aluminum or some superalloy, or a 300 series stainless..  Aluminum would be  preferable because of its high strength/.weight though its superb thermal conductivity turns out to be a mixed blessing.  A high temperature superalloy is second choice, though a lower strength/weight hurts doubly,  in the conventional way, it weighs more thus reducing thrust/weight, but much more importantly, it can't be spun as fast, thus reducing the chamber pressure possible.  We may end up using a 300 series stainless because it has good cryo properties and good strength at cryo temperatures, where the bulk of the engine will be operating.  Note however that as thrust/weight exceeds 200:1 further improvement starts to get lost in the noise, at least for my system design, as confirmed by my simulator.  This and the desire for fast  prototype turn around precludes using any hitech ceramic or other exotic materials. However, there are other options for the center piece, the "spindle", if the thermal requirements on cooling the nozzles are too much it could be made of a machinable ceramic or tungsten, or elconite, or graphite or something.  Thermal coefficients of expansion, thermal conductivity and such may override strength and strength/weight factors for the spindle, it doesn't have nearly the same forces on it as the rotor does.

NOTE: about this set of calculations:
    this stuff is meant to be a formalization of my calculations for several purposes.  There are several semiemperical equations here from Sutton and other sources if there are any better formulas or methods, I want to know about them, so this is for review.  Also I expect to run this on a lot of configurations, both manually to develop an intuition, and as part of my rocket system simulator, to explore optima and trade-offs.  In particular, there may be temperature:ISP trade-offs, the simulator can integrate those into an entire system.  As real engines burn, both success and failure will give values and directions to the simulator(s).  The current simulator flies a rocket second by second a 100,000 times under an adaptive simulated annealer, a variety of numerical hill climbing algorithm.  The addition of this engine calculation along with an interface to chemical calculations will give a more complete model, and the addition of manufacturing cost rules of thumb can lead to trade-offs between manufacturing costs, of the engine for instance, and the fuel mix, for temperature and ISP, which will define tankage ratios & etc.  If this design isn't in an unexplored realm of design space, it isn't worth investigating, and if it is unexplored as I expect, normal intuitions will be misleading!

    measurements in meters& SI unless otherwise noted:  The physics makes a lot more sense in SI even though I have less feel for results in Newtons than in pounds force (lbf).  And I still don't use Pascals for everyday pressure measurements.  So sometimes I output in the more intuitive units as well as the SI units.  One has to learn somehow.  Without some discipline in this the units can cause a lot of mayhem to the results or at least sanity.

geometry

Geometry
$RowBox[{superalloy, , thrust = , , 3000, , chht , , 0.0293422, , vol in^3 = , , 4.84316}]$

rBot	Wall	stress lbf	sp thrust	weight	dia	dia ft	r max stress	min # noz	max # noz
0.0173205	0.00144225	RowBox[{RowBox[{267629., }], +, RowBox[{113784., , i}]}]	773.843	3.87676	0.09621	0.320195	RowBox[{RowBox[{0.0210481, }], -, RowBox[{0.0210481, , i}]}]	0	0
0.0173205	0.00216337	190624.	748.827	4.00627	0.0976522	0.324995	0.0201087	0	0
0.0173205	0.0028845	127674.	725.387	4.13573	0.0990945	0.329795	0.0285541	0	0
0.0173205	0.00360562	100552.	703.388	4.26507	0.100537	0.334595	0.0315264	0	0
0.0173205	0.00504787	75251.1	663.255	4.52315	0.103421	0.344195	0.0344412	0	0
0.0173205	0.005769	68820.5	644.918	4.65175	0.104863	0.348994	0.0353455	0	0
0.0173205	0.00649012	64529.4	627.618	4.77998	0.106306	0.353794	0.0360782	0	0
0.0173205	0.00721125	61701.	611.276	4.90777	0.107748	0.358594	0.0366991	0	0
0.0173205	0.00793237	59924.1	595.823	5.03505	0.10919	0.363394	0.0372428	0	0
0.0173205	0.0086535	58933.9	581.196	5.16177	0.110632	0.368194	0.0377308	0	0
0.0173205	0.00937462	58552.2	567.339	5.28785	0.112075	0.372994	0.0381772	0	0
0.0173205	0.0100957	58654.7	554.198	5.41323	0.113517	0.377794	0.0385917	0	0
0.0173205	0.0108169	59151.7	541.727	5.53784	0.114959	0.382594	0.038981	0	0
0.0173205	0.011538	59977.5	529.883	5.66163	0.116401	0.387394	0.03935	0	0
0.0173205	0.0122591	61082.2	518.626	5.78452	0.117844	0.392194	0.0397024	0	0

RowBox[{, RowBox[{thicknessOfChamberWall=. ;, , x=. ;, , rBot=. ;, , , lEngine = combustionChamberLength + 2 thicknessOfChamberWall/.geometry ;}]}]

$RowBox[{720.306, , Null^49, , (-1500 + TEngineHotFluid)}]$

RowBox[{ , RowBox[{lfuelfeeds = .73 lEngine ;, , lprimaryfeed = .47 lEngine ;, <br ... specificThrust/.Join[geometry, fuel, oxidizer, velocity, superalloy] ;, , Null}]}]

$RowBox[{nominalFuelFlowMass = , , RowBox[{RowBox[{(, RowBox[{0.0001683, , combustionChamberHeight^3, , densityFuel, , rotationalVelocity^2}], )}], /, lStar}]}]$

$RowBox[{0.0096012, , l, , Null^72}]$

volapprroxcone = 1/3 π (rBot + combustionChamberHeight + thicknessOfChamberWall + lTop/2) ... l, oxidizer, velocity, geometry] ; Print["totalvol= ", totalvol/.geometry] ; 

Print["nTubesInner = ", nTubesInner/.geometry/.geometry] ; Print["nTubesOuter ... }], , /., , geometry}], /., fuel}], /., oxidizer}], /., velocity}]}], ]}], ;}], }] Null

$RowBox[{volumeOfSpindleTubes = , , 2.41319*10^-6}]$

$RowBox[{volumeOfRotorTubes = , , 7.23958*10^-6}]$

$RowBox[{volumes: engine_combustionchamber = , , 0.00008896}]$

$RowBox[{ m^3 volumes: spindle = , , 0.0000370667, , volumes: rotor =, , 0.0000518933}]$

$RowBox[{CalculatedNozzleThroat Area = , , 0.000646982, , , , 1.00282, , in^2}]$

$RowBox[{chamberPressure = , , 3.7044*10^7}]$

Chemistry

TLox = 90 ; TPropane = 90 ; molWeightPropane = 44 ; molWeightO2 = 32 ; molWeightS ... izer, velocity] ; Print["nominalFuelFlowMass ", localnominalFuelFlowMass] ; Null

$RowBox[{nominalFlowMasspropane = , , RowBox[{RowBox[{(, RowBox[{0.0000597192, , combustionChamberHeight^3, , densityFuel, , rotationalVelocity^2}], )}], /, lStar}]}]$

$RowBox[{nominalFlowMassLOX = , , RowBox[{RowBox[{(, RowBox[{0.00010858, , combustionChamberHeight^3, , densityFuel, , rotationalVelocity^2}], )}], /, lStar}]}]$

Pressure

pressureFuelInjector = (rotationalVelocity^2) densityFuel/2 /.Join[geometry, fuel, oxidi ... ure/.fuel/.velocity, " (", chamberPressure/(100000/15)/.fuel/.velocity, ")"] ;

$RowBox[{Oxidizer pressure drop , , 6.3504*10^7, , (, , 9525.6, , )}]$

$RowBox[{fuel pressure drop , , 2.4696*10^7, , (, , 3704.4, , )}]$

$RowBox[{ChamberPressure = , , 3.7044*10^7, , (, , 5556.6, , )}]$

cavitation

Cavitation

fuel_velocities

graphics

Graphics TubesToChamberWallInnerTop TubesToChamberWallInnerBot TubesToChamberWallOuterTop TubesToChamberWallOuterBot

RowBox[{ , RowBox[{l5ths = .000240 ;, , RowBox[{RowBox[{g1, , =, , RowBox[{RowBox ... , Show[g1, gttp , gtto, lttp, ltto, ito, itp, gm1, gm2, AspectRatio-> Automatic] ;}]}]

[Graphics:HTMLFiles/xxrocket_heatfeb15_2004htmlized_82.gif]

Show[g2, ltbo, ltbp, llube, lnozzle, ligniter, AspectRatio-> Automatic] ; 

[Graphics:HTMLFiles/xxrocket_heatfeb15_2004htmlized_85.gif]

computationforcad

$calctubes[ntubesb_, z0lineb_] := Module[{resultb, thetab, tmpb, ib}, (*Print[z0line] ; *)(*Pri ... quot;, resultb] ; *)] ; (*Print[resultb] ; *)Return[resultb] ; ] ;$

(*foobar0 = calctubes[nTubesInner, lltbo] ; foobar1 = calctubes[nTubesInner, lltbp] ; ... , lltbo]] ; *)Null

generate_cad

nTubesOuter = 30 ; nTubesInner = 10 ; rotorandspindleozygenedgedisplacem ... radiusLOX] ;  (*lltbo, lltbp, llttp, lltto *)Print["foo23"] ;

$injectorradius =  {{iNJECTORRADIUS -massflow^(1/2)/(2^(1/4) (densityoffluid pd ... /2))}, {iNJECTORRADIUSmassflow^(1/2)/(2^(1/4) (densityoffluid pdrop)^(1/4) π^(1/2))}}$

$RowBox[{(*derived from picture as above*), , RowBox[{(*, ... "\"", ")\n"] ; ] ; ] ; }]$

first the rotor

$Close[rogersfile] ; rogersfile = OpenWrite["/roger/cadstartrotornew1.lsp"] ; savedou ... WriteString[rogersfile, "(Command \"-view\" \"top\")\n"] ; $

$RowBox[{RowBox[{(*, RowBox[{RowBox[{g2, , =, RowBox[{RowBox[{Graphics, [, RowBox[{{, RowBox[{ ... String[rogersfile, "(Command \"-view\" \"top\")\n"] ; Null}]$

propanemanafoldoffset = (lOverlap - 2^(1/2) TubesToChamberWallOuterBot - rTubesInner)/.geometry ; loxmanafoldoffset = lEngine - propanemanafoldoffset ;

spheresin = 2 (rTubesInner/rInner)/.geometry ; sphereangle = (360/(2Pi)) ArcSin[spheresin] ; R ... t;, manafoldangle] ; Print["2rTubesInner/rInner = ", (2rTubesInner/rInner)/.geometry] ;

$Close[rogersfile] ; rogersfile = OpenWrite["/roger/cadstartmanifoldprop.lsp"] ; save ... file, "(Command \"-view\" \"top\")\n"] ; Close[rogersfile] ;$

$rogersfile = OpenWrite["/roger/cadstartmanifoldlox.lsp"] ; savedoutput = $Output ; W ... mmand \"-view\" \"top\")\n"] ; Close[rogersfile] ;  $

Outer feed tube

$RowBox[{RowBox[{clearance3ths, , =, , RowBox[{.003, , /, RowBox[{(, RowBox[{100, /, 2.54}], ... le, "(Command \"-view\" \"top\")\n"] ;  Close[rogersfile] ;$

$rogersfile = OpenWrite["/roger/cadstartinnerfeed.lsp"] ; savedoutput = $Output ; Wri ... le, "(Command \"-view\" \"top\")\n"] ;  Close[rogersfile] ;$

$rogersfile = OpenWrite["/roger/cadstartouterinducer.lsp"] ; savedoutput = $Output ; ... file, "(Command \"-view\" \"top\")\n"] ; Close[rogersfile] ;$

$rogersfile = OpenWrite["/roger/cadstartinnerinducer.lsp"] ; savedoutput = $Output ; ... file, "(Command \"-view\" \"top\")\n"] ; Close[rogersfile] ;$

$rogersfile = OpenWrite["/roger/cadstartstator.lsp"] ; savedoutput = $Output ; WriteS ... le, "(Command \"-view\" \"top\")\n"] ;  Close[rogersfile] ;$

$rogersfile = OpenWrite["/roger/cadstartseal.lsp"] ; savedoutput = $Output ; WriteStr ... file, "(Command \"-view\" \"top\")\n"] ; Close[rogersfile] ;$

Nozzlenozzle design objectives, an noncircular nozzle which can be til ... f s^n = x ^n + y^n n>2rnozzlecenterInnerrNozzlesthroat

$RowBox[{, RowBox[{rogersfile = OpenWrite["/roger/cadstartnozzlesuperelipse.lsp&qu ... 371;, WriteString[rogersfile, "(entmake '((0 . \"SEQEND\")))\n"] ;, }]}]$

Close[rogersfile] ;  

RowBox[{RowBox[{RowBox[{g2, , =, RowBox[{RowBox[{Graphics, [, RowBox[{{, RowBox[{RowBox[{RGBC ... , {lprimaryfeed, rprimaryfeed}, {0, rprimaryfeed}}]}], }}], ]}], /., geometry}]}], ;}], }]

Fuel_Flow

$RowBox[{, RowBox[{outsidearesecondaryfeedtube = π rsecondaryfeed^2 ; insi ... ichO2 = ", volRichO2] ;, , Print["volRichPropane = ", volRichPropane] ;}]}]$

$RowBox[{static pressure of lox velocity = , , RowBox[{RowBox[{(, RowBox[{2.97195*10^-7 ... 015}], +, RowBox[{0.4, , combustionChamberHeight}]}], )}], ^, 2}], , π}]}], )}], ^, 2}]}]}]$

$RowBox[{loxflowvelocity = , , RowBox[{0.000770966, /, RowBox[{RowBox[{(, RowBox[{RowBo ... [{-, 0.0015}], +, RowBox[{0.4, , combustionChamberHeight}]}], )}], ^, 2}], , π}]}], )}]}]}]$

outareainnerfeedtube = π (rinnerfeed)^2 ; insidearesecondaryfeedtube = &# ... feed->rprimaryfeed/.geometry] ; Print["xevary = ", xevary] ; 

$RowBox[{xevary = , , RowBox[{{, RowBox[{RowBox[{{, RowBox[{rinnerfeed, , RowBo ... ^2}], -, RowBox[{1., , thicknessofinnerfeedtube^2}]}], )}], ^, (1/2)}]}]}], )}]}]}], }}]}], }}]}]$

structural

Structural

I don't have all the answers here.  I need closed form solution here, as this is meant to be part of a adaptive annealing simulator, and will be evaluated for different values of all the structural parameters, and different fuel mixes.So I need a closed form solution, as it will be evaluated 100,000 times a run for hundreds or thousands of runs. Due to the simplicity of this design, there should be a closed form solution, but till I learn how to do that, I'll look for upper and lower bounds.

The expected failure modes are strains sufficient to separate the rotor from the spindle, and stresses sufficient to cause rotor failure. The intent is to use a thermal shrink interference fit to join the two.

The first approximation is to look at various stresses on radial disks, ignoring the torsional component that would tie things together.
    Stresses for the pressure component are given by the Lamé equations
    = (r_1 ^(2 ) p_1 )/(r_2 ^(2 ) - r_1 ^(2 )) (1+)
     = (1-)
    Stresses for the rotational component are
    σ=ρ(- (r_2^2 r_1^2)/r^2 - )
    σ=ρ( $FormBox[RowBox[{r_2^2, , +, , r_1^2, -, (r_2^2 r_1^2)/r^2, -, RowBox[{RowBox[{RowBox[{(, RowBox[{1, +, RowBox[{3., μ}]}], )}], /, (3 + μ)}], r^2}]}], TraditionalForm]$ )

    We will look at the stresses on the interior edge of a disk at the edge of the rotor looking for the strain that
    will cause the two pieces to separate. (Note that I'm cheating here, there isn't pressure there, but this is a good start, upper bound to speed.)

$Sr = (r1^2 p )/(r2 ^(2 ) - r1^2) (1 - (r2 ^(2 ))/(r ^(2 ))) St = (r_1 ^(2 ) p )/(r2 ^(2 ) - ... +, RowBox[{3., μ}]}], )}], /, (3 + μ)}], r^2}]}], TraditionalForm], )}]}], Text]}], ;}]$

So using these at the interior edge where r = rInner, first we set the stresses to the interference pressure:

But we may have better use for the radial elongation form of this stuff, as that is likely the ... + (3 + μ)/8 ρ ω^2 (r2^2 + r1^2 - (r2^2 r1^2)/r^2 - r^2)) (1 - μ)/elasticity ;

ω=. ; radialelongation=. ; modulusElasticity=. ; μ=. ; ρ=. ; r=. ; p=. ; ω ... 2 ((r2^2 + r1^2) - (r2^2 r1^2)/r^2 - r^2)) (1 - μ))/(8 modulusElasticity), ω]] ;

ros = rotationsolution [[1]]/.{r1 rInner, ρdensity, radialelongation > ... nner + linterference, r2  rOuter}/.geometry/.fuel/.oxidizer/.stainlesssteel420/.velocity ;

ros = rotationsolution [[1]]/.{r1 rInner, ρdensity, radialelongation > ... linterference, r2  rOuter}/.Join[geometry, fuel, oxidizer, stainlesssteel420, velocity] ;

(*`maxtstressformula = (( (r1 p wallchamberratio)/modulusElasticity ((1 + r1^2/r2^2)/(1 - r1^2 ... ;^2 (r2^2 + r1^2 - (r2^2 r1^2)/r^2 - r^2))) * modulusElasticity * (r1^2 + r2^2)/(4r1 * r2^2)) ; *)

maxtstressformula = ((r1^2 p wallchamberratio)/(r2^2 - r1^2) (1 + r2^2/r^2) + ((3 + μ)/8 ρ ω^2 (r2^2 + r1^2 - (r2^2 r1^2)/r^2 - r^2)) (1 - μ)) ;

minmaxr = Solve[0 == D[maxtstressformula, r], r] ; Null

maxr = minmaxr[[4]][[1]] ; (*/.{r1 rInner, pchamberPressure, & ... t; rotationalVelocity/rInjector }/.Join[geometry, fuel, oxidizer, stainlesssteel420, velocity]] *)

samaxtstress = maxtstressformula /.{r1 rInner, pchamberPressure, μ ... > rotationalVelocity/rInjector }/.Join[geometry, fuel, oxidizer, stainlesssteel420, velocity] ;

$RowBox[{RowBox[{1.36204*10^8, /, 6894.7}], }]$

with impellers to pre pressurize itwe get a bit more, that can be added as it is de ... side . Note that the result is for some steel, for aluminum the answer is similar 

ω =. ; radialelongation = . ; modulusElasticity =. ; μ = . ; ρ = . ; r &nb ... 62754;rInner + linterference, r2  rOuter}/.geometry/.fuel/.oxidizer/.aluminum/.velocity ;

almaxstress = maxtstressformula/.{r1 rInner, p chamberPressure, μ ... p;ω-> rotationalVelocity/rInjector }/.Join[geometry, fuel, oxidizer, aluminum, velocity] ;

The stresses on the center of the rotor will show us the speed where the rotor fails by flying apart, again ignoring shear effects. We use the interferencePressure formula, but use the outer edge and a failure stress !

Now, and more interestingly, we look at the tangential pressure components integrated over the area of the chamber wall + the tangential stresses integrated along the length of the rotor. .... how close is this to a solution... ...rigid ia an Pyrex... how close are we to integrating real torsion to this ....

thermal

Thermal

Cold_Cooling_side

couldside_boundarylayer_forced

Note for the first cut this is the same equation as the hot side cooling, the parameters are different as is the geometry . This is the physical effect that cools other rocket engines, and is included here to confirm that this effect won't cool this engine as designed. See the convection section for the actual effect that works.

Cooling Cold sideFor the amount of heat transferred from cold tubes we will start with
the approximation of constant temperature of the metal wall. I will use Q = π∫DqdL
and h = $FormBox[RowBox[{(, RowBox[{RowBox[{cpμ, ^, 0.2}], /, RowBox[{Pr, ^, 0.6}]}], )}], TraditionalForm]$ $FormBox[RowBox[{(ρμ), ^, 0.8}], TraditionalForm]$
equations (8-20) & (8-23) from Sutton 7th ed. My intuition fails me here without a good reference.

ρlocal =. ; cp = . ; ρam=. ; & ... 6;0=. ; μlocal=. ; thermalConductivity =. ; Pr=. ;

TEngineWall=. ; TEngineWallChamber=. ; TEngineWallInner=. ; RowBox[{TFluid =., ;, RowBox[{? ... alConductivity.21}], }}]}], ;, , Pr = (cp μlocal)/thermalConductivity, ;}]}]}]

plysics_cold_forced_convection

$physics cold forced convection RowBox[{RowBox[{Qabstract, =, RowBox[{π, , 2^(1/2), , tu ... meter^.2, , RowBox[{Pr, ^, 0.6}], , ρprime, , μ0^.2}], )}]}], r}]}]}]}], ;}]$

QinnerLOX = Qabstract/.fuelfeedvelocityflowRateInnerLox/.arTop ... opane + Qouterpropane ; QLOX = QinnerLOX + Qouterlox ; Qpropane = Qinnerpropane + Qouterpropane ;

qperkey1

tubeallltemperature = 300 ; qPerKey = Q/nominalFuelFlowMass ; qPerKeyLOX = QLOX/(O2WeightRich ... erturerises due to cold forced convection see free convection for real temp rises"] ;

qperkey1

couldside_boundarylayer_free

RowBox[{, RowBox[{Cold boundary layer dominated by free convection, , &n ... , , www . egr . msu . edu/~ somerton/Nusselt/index . html}], ;}]}], , Null}]}]

thicknessToCoolantEngine=. ; TDelta = 5 ; μ=. ; ν = μ/ρ ; Pr = (cp ... Ra = Gr Pr ; Gz = (Ren Pr D)/L ; Ren = (V D)/μ ; Pr = (cp μ)/thermalConductivity ; Null

μ=. ; ϕ=. ; ν = μ/ρ ; Pr = (cp μ)/thermalConductivity ;

physics_cold_free_convection

(* key physics cold free convection *) GrL = (geffective β (TDelta) L^3)/ν^2 ; GrD = (geffective β (TDelta) D^3)/ν^2 ;

physics_cold_free_convection

Null

RaL = GrL Pr ; RaD = GrD Pr ; GzD = (RenD Pr D)/L ; RenD = (V D)/μ ; RenL = (V L)/μ ; Pr = (cp μ)/thermalConductivity ;

$RowBox[{NuavL, =, RowBox[{1, +, RowBox[{1.44, , *, Max[0, 1 - 1798/(Ra Cos[ϕ])], , RowB ... 1.6}]}], )}], /, (Ra Cos[ϕ])}]}], )}]}], +, Max[0, ((Ra Cos[ϕ])/5830)^(1/3) - 1], }]}]$

ω = rotationalVelocity/rInjector/.geometry/.velocity ; 

RowBox[{NuavL, =, RowBox[{1, +, RowBox[{1.44, *, Max[0, 1 - 1798/(RaL Cos[ϕ])], , RowBox ... 04;LOXcharisterics/.geometry] ; Print["doublecheck RaD = ", grdlocal prlocal] ;

$RowBox[{1, +, RowBox[{Max, [, RowBox[{0, ,, RowBox[{-1, +, RowBox[{41.6737, , ((cp L^3 r ` ... owBox[{Sin, [, RowBox[{1.8, , ϕ}], ]}], ^, 1.6}]}], )}], /, (cp L^3 r ρ^2)}]}], )}]}]}]$

$RowBox[{Part 1 = , , RowBox[{1, -, RowBox[{1.57681*10^-14, /, r}]}]}]$

$RowBox[{Part 2 = , , RowBox[{1, -, RowBox[{1.54587*10^-14, /, r}]}]}]$

$RowBox[{Part 3 = , , RowBox[{-1, +, RowBox[{26943.1, , r^(1/3)}]}]}]$

$RowBox[{hpermsqLOXouter = , , RowBox[{53.5433, , RowBox[{(, RowBox[{1, +, RowBox[{1.4 ... +, RowBox[{Max, [, RowBox[{0, ,, RowBox[{-1, +, RowBox[{26943.1, , r^(1/3)}]}]}], ]}]}], )}]}]}]$

$RowBox[{hLOXouter = , , RowBox[{1.72659, , RowBox[{(, RowBox[{1, +, RowBox[{1.44, , ... +, RowBox[{Max, [, RowBox[{0, ,, RowBox[{-1, +, RowBox[{26943.1, , r^(1/3)}]}]}], ]}]}], )}]}]}]$

$RowBox[{hpermsqLOXinner = , , RowBox[{53.5433, , RowBox[{(, RowBox[{1, +, RowBox[{1.4 ... +, RowBox[{Max, [, RowBox[{0, ,, RowBox[{-1, +, RowBox[{26943.1, , r^(1/3)}]}]}], ]}]}], )}]}]}]$

$RowBox[{hLOXinner = , , RowBox[{0.575531, , RowBox[{(, RowBox[{1, +, RowBox[{1.44, , ... +, RowBox[{Max, [, RowBox[{0, ,, RowBox[{-1, +, RowBox[{26943.1, , r^(1/3)}]}]}], ]}]}], )}]}]}]$

$RowBox[{hpermsqpropaneouter = , , RowBox[{66.1417, , RowBox[{(, RowBox[{1, +, RowBox[ ... +, RowBox[{Max, [, RowBox[{0, ,, RowBox[{-1, +, RowBox[{8349.62, , r^(1/3)}]}]}], ]}]}], )}]}]}]$

$RowBox[{hpropaneouter = , , RowBox[{2.13285, , RowBox[{(, RowBox[{1, +, RowBox[{1.44, ... +, RowBox[{Max, [, RowBox[{0, ,, RowBox[{-1, +, RowBox[{8349.62, , r^(1/3)}]}]}], ]}]}], )}]}]}]$

$RowBox[{hpermsqpropaneinner = , , RowBox[{66.1417, , RowBox[{(, RowBox[{1, +, RowBox[ ... +, RowBox[{Max, [, RowBox[{0, ,, RowBox[{-1, +, RowBox[{8349.62, , r^(1/3)}]}]}], ]}]}], )}]}]}]$

$RowBox[{hpropaneinner = , , RowBox[{0.71095, , RowBox[{(, RowBox[{1, +, RowBox[{1.44, ... +, RowBox[{Max, [, RowBox[{0, ,, RowBox[{-1, +, RowBox[{8349.62, , r^(1/3)}]}]}], ]}]}], )}]}]}]$

$RowBox[{convectionQ = , , RowBox[{RowBox[{2.8438, , RowBox[{(, RowBox[{1, +, RowBox[{ ... , RowBox[{Max, [, RowBox[{0, ,, RowBox[{-1, +, RowBox[{26943.1, , r^(1/3)}]}]}], ]}]}], )}]}]}]}]$

$RowBox[{NuavLLOX = , , RowBox[{1, +, RowBox[{1.44, , RowBox[{(, RowBox[{1, -, RowBox[ ... ]}]}], +, RowBox[{Max, [, RowBox[{0, ,, RowBox[{-1, +, RowBox[{26943.1, , r^(1/3)}]}]}], ]}]}]}]$

$RowBox[{NuavLpropane = , , RowBox[{1, +, RowBox[{1.44, , RowBox[{(, RowBox[{1, -, Row ... ]}]}], +, RowBox[{Max, [, RowBox[{0, ,, RowBox[{-1, +, RowBox[{8349.62, , r^(1/3)}]}]}], ]}]}]}]$

$RowBox[{GrL = , , RowBox[{5.81105*10^16, , r}]}]$

$RowBox[{GrD = , , RowBox[{1.85774*10^14, , r}]}]$

$RowBox[{RaD = , , RowBox[{5.15533*10^14, , r}]}]$

$RowBox[{doublecheck RaD = , , RowBox[{5.15533*10^14, , r}]}]$

$RowBox[{1, +, Max[0, -1 + ((geffective L^3 (RDelta) β ρ^2 Cos[ϕ] cp)/(thermalCo ... 8, , ϕ}], ]}], ^, 1.6}]}], )}], /, (geffective L^3 (TDelta) β ρ^2 cp)}]}], )}]}]}]$

$RowBox[{1, +, RowBox[{Max, [, RowBox[{0, ,, RowBox[{-1, +, RowBox[{24.371, , ((cp L^3 r RDelt ... owBox[{Sin, [, RowBox[{1.8, , ϕ}], ]}], ^, 1.6}]}], )}], /, (cp L^3 r ρ^2)}]}], )}]}]}]$

cooling_hotside

cooling hotside free Null

hotside_free

The hotside also has significant accereraton and thus the free convection effects there must b ... stance so it is acceptable to use aflat slopeing plate as the appropriate model . 

TEngineWallChamber=. ; TEngineWallInner=. ; r=. ; qlocal =. ; μ=. ; ϕ=. ; RowBox[{Ro ... ; RaL = GrL Pr ; RaD = GrD Pr ; GzD = (RenD Pr D)/L ; RenD = (V D)/μ ; RenL = (V L)/μ ;

physics hot free convection

$RowBox[{(* key equation hot boundary layer *), , StyleBox[RowBox[{RowBox[{NuL, , =, , ... 8/27)}], )}], ^, 2}], /, 2^(1/2)}]}], ;}], FontColor -> RGBColor[0.0195315, 0.410163, 0.121096]]}]$

Print[" NuL = ", NuL, "qabstractfreehotside = ", qabstractfreehotside ] ; ... rint[" NuL = ", NuL, "qabstractfreehotside = ", qabstractfreehotside ] ; Null

$RowBox[{ NuL = , , RowBox[{RowBox[{RowBox[{(, RowBox[{RowBox[{0.825, }], +, Ro ... }], +, RowBox[{4860., , (L^3 r (TEngineHotFluid - TEngineWallChamber))^(1/6)}]}], )}], ^, 2}]}]}]$

$RowBox[{RaL = , , RowBox[{2.69075*10^20, , L^3, , r, , (TEngineHotFluid - TEngineWallChamber)}]}]$

$RowBox[{ NuL = , , RowBox[{RowBox[{RowBox[{(, RowBox[{RowBox[{0.825, }], +, Ro ... , +, RowBox[{4315.22, , (L^3 r (TEngineHotFluid - TEngineWallChamber))^(1/6)}]}], )}], ^, 2}]}]}]$

hotsidemixed, hotside_forced

TEngineWallChamber=. ; TEngineWallInner=. ; nominalcombustantsvelocity = 0 ;  qlocal =. ;

RowBox[{RowBox[{If, [, RowBox[{False, ,, (* 420m/s 5000psi case *), , RowBox[{TChamber ... #961;local, ;}], , (* density at freestream *), , ,}], ]}], ;}], , }] Null

$ chamberPressure = .6 * (densityFuel * rotationalVelocity^2)/2 ; velocity = {rotationalVelocity -> nominalrotationvelocity} ;$

fakePr = (cp μlocal)/gasthermalConductivity ; rATr = combustionChamberHeight/2 ; Print["Pr = ", Pr, " fakepr = ", fakePr] ;

physics_hot_boundary_layer_forced_convection

key physics hot boundary forced convection from Sutton  (rTop/r) is the s ... up due to conservaton of angular monemtum as the gas goes to the center . 

keycoolingequation

RowBox[{RowBox[{velocityexpression = ((rTop/r - r/rTop)) ;, , StyleBox[RowBox[{RowBox[ ... .410163, 0.121096]], , , qabstractforcedhotside = qabstractforcedhotside1 ;}], }]

... ;rATr = combustionChamberHeight/2 ; geffective = ω^2r ; tmpT = 1500 ;

$RowBox[{qabstractforcedhotside1, , RowBox[{RowBox[{(, RowBox[{268.043, , RowBox[{(((3 ... alVelocity), ^, 0.8}], , TEngineHotFluid}], )}], /, RowBox[{combustionChamberHeight, ^, 0.2}]}]}]$

$RowBox[{qabstractforcedhotside2, , RowBox[{RowBox[{(, RowBox[{268.043, , RowBox[{(((3 ... , (TEngineHotFluid - TEngineWallChamber)}], )}], /, RowBox[{combustionChamberHeight, ^, 0.2}]}]}]$

$RowBox[{qabstractforcedhotside1, , RowBox[{RowBox[{(, RowBox[{271.586, , RowBox[{(((3 ... , (TEngineHotFluid - TEngineWallChamber)}], )}], /, RowBox[{combustionChamberHeight, ^, 0.2}]}]}]$

$RowBox[{qabstractforcedhotside2, , RowBox[{RowBox[{(, RowBox[{149.738, , RowBox[{(((3 ... , (TEngineHotFluid - TEngineWallChamber)}], )}], /, RowBox[{combustionChamberHeight, ^, 0.2}]}]}]$

RowBox[{RowBox[{smellyconstant, , =, , RowBox[{RowBox[{RowBox[{RowBox[{RowBox[{RowBox[{RowBo ... Print["smellyconstant = ", smellyconstant] ; Print["smellyhg = ", smellyhg] ;

$RowBox[{tmp0 complete = , , 1.99833*10^6}]$

$RowBox[{tmp1 complete = , , 1.99833*10^6}]$

$RowBox[{tmp6 (TEngineHotFluid-TEngineWallChamber) (cp ) = , , 3.3167*10^6}]$

$RowBox[{qabstract mid = , , 1.64812*10^8}]$

$RowBox[{qabstract bot = = , , 4.16958*10^8}]$

(*Qfree = 2 π 2^(1/2) ∫_arBot^arTopr qabstractfreehotside r/.geometry ; *)& ... 54;tmpT/.L-> arTop - arBot/.arToprTop/.arBotrBot/.geometry ; *)

$RowBox[{ggfake value = , , RowBox[{2, , 2^(1/2), , π, , RowBox[{(, ... (-arBot + arTop), , combustionChamberHeight, , RowBox[{rotationalVelocity, ^, 0.8}]}]}], )}]}]}]$

(*Qforcedpersqm = smellyconstant * ggfhq ; Qforced = Qforcedpersqm * (areaOfCo ... elocity]/.TEngineHotFluidTChamberHotGasChamber/.TEngineWallChambertmpT] ; 

$RowBox[{ggfhq = , , RowBox[{2, , 2^(1/2), , π, , RowBox[{(, RowBox[{RowBox[{Ro ... (-arBot + arTop), , combustionChamberHeight, , RowBox[{rotationalVelocity, ^, 0.8}]}]}], )}]}]}]$

$RowBox[{Qforced = , , RowBox[{6316.96, , RowBox[{(, RowBox[{RowBox[{RowBox[{(, RowBox ... combustionChamberHeight, , RowBox[{rotationalVelocity, ^, 0.8}]}]}], )}], , TEngineHotFluid}]}]$

$RowBox[{Q = , , RowBox[{6316.96, , RowBox[{(, RowBox[{RowBox[{RowBox[{(, RowBox[{2, ... combustionChamberHeight, , RowBox[{rotationalVelocity, ^, 0.8}]}]}], )}], , TEngineHotFluid}]}]$

$RowBox[{value of Qforced = , , 1.61008*10^6}]$

$RowBox[{value of Q = , , 1.61008*10^6}]$

$RowBox[{Q = , , 1.61008*10^6}]$

$RowBox[{Q inner , , 1.15005*10^6}]$

temperaturerise

<a href= Calculations of temperature rise in LOX and propane" width="706" height="47" align="absmiddle" />

qperkey2

RowBox[{, RowBox[{Print["O2WeightRich = ", O2WeightRich] ;, , ᡝ ... er, velocity]/.TEngineHotFluidTChamberHotGasChamber/.TEngineWallChambertmpT] ;}]}]

qperkey2

$RowBox[{O2WeightRich = , , RowBox[{RowBox[{(, RowBox[{0.00010858, , combustionChamberHeight^3, , densityFuel, , rotationalVelocity^2}], )}], /, lStar}]}]$

qperkey2

$RowBox[{propaneWeightRich = , , RowBox[{RowBox[{(, RowBox[{0.0000597192, , combustionChamberHeight^3, , densityFuel, , rotationalVelocity^2}], )}], /, lStar}]}]$

qperkey2

$RowBox[{ per sqmeter LOX = , , 4.87598*10^7}]$

qperkey2

$RowBox[{nominalFuelFlowMass = , , RowBox[{RowBox[{(, RowBox[{0.0001683, , combustionChamberHeight^3, , densityFuel, , rotationalVelocity^2}], )}], /, lStar}]}]$

qperkey2

$RowBox[{O2WeightRich = , , RowBox[{RowBox[{(, RowBox[{0.00010858, , combustionChamberHeight^3, , densityFuel, , rotationalVelocity^2}], )}], /, lStar}]}]$

qperkey2

RowBox[{RowBox[{RowBox[{thermalconductivitymetal, , =, , 15.7}], ;}], , }] Print[ & ... t;, qamid ] ; Print[ "qabstract bot = = ", qabot ] ;

qperkey2

$RowBox[{qabstract mid = , , 1.64812*10^8}]$

qperkey2

$RowBox[{qabstract bot = = , , 4.16958*10^8}]$

qperkey2

qPerKeypropane = localq/(nominalFuelFlowMass propaneWeightRich) ; localq ... O2/cplox/.TEngineHotFluidTChamberHotGasChamber/.TEngineWallChambertmpT] ; 

qperkey2

nozzle_thermal_transfer

TEngineWallChamber=. ; TEngineWallInner=. ; qlocal =. ; μ=. ; ϕ=. ; RowBox[{RowBox[{ ... ρam ; β = 1 ;  Print["RaL = ", RaL] ; Print["Pr = ", Pr] ;

$RowBox[{RaL = , , RowBox[{2.69075*10^20, , L^3, , r, , (TEngineHotFluid - TNozzle)}]}]$

nozzleAnglesubsonic = 45 π/180 ; nozzleAnglesupersonic = 15 π/180 ; doo = &nbs ... (nozzlevelocity[l, nozzleAnglesubsonic, nozzleAnglesupersonic]), ^, 0.8}]}], , )}]}], )}]}], ;}]

Print["qnozzleqabstractforced = ", qnozzleqabstractforced] ; (* integrate ov ... ernozzleheat /.geometry/.metal] ; Print["nozzleheat = ", nozzleheat/.geometry/.metal] ;

cooling_combined

(*Print["goodness ratio = ",localconvectionQ/localqPerKeyhot/.geometry ];

Solve [localqPerKeyhot == - localconvectionQ/.TDelta ->2]
Solve [localqPerKeyhot ==- localconvectionQ/.TEngineWallInner->103/.TFluid ->100,TEngineWallChamber]
Solve [localqPerKeyhot == - localconvectionQ/.TEngineWallInner->104/.TFluid ->100,TEngineWallChamber]
Solve [localqPerKeyhot == -localconvectionQ/.TEngineWallInner->105/.TFluid ->100,TEngineWallChamber]
Solve [localqPerKeyhot == -localconvectionQ/.TEngineWallInner->106/.TFluid ->100,TEngineWallChamber]
Solve [localqPerKeyhot == -localconvectionQ/.TEngineWallInner->107/.TFluid ->100,TEngineWallChamber]
Solve [localqPerKeyhot ==- localconvectionQ/.TEngineWallInner->108/.TFluid ->100,TEngineWallChamber]
Solve [localqPerKeyhot ==- localconvectionQ/.TEngineWallInner->109/.TFluid ->100,TEngineWallChamber]
Solve [localqPerKeyhot ==- localconvectionQ/.TEngineWallInner->110/.TFluid ->100,TEngineWallChamber]
Solve [localqPerKeyhot ==- localconvectionQ/.TEngineWallInner->111/.TFluid ->100,TEngineWallChamber]
Solve [localqPerKeyhot == -localconvectionQ/.TEngineWallInner->112/.TFluid ->100,TEngineWallChamber]
Solve [localqPerKeyhot ==- localconvectionQ/.TEngineWallInner->113/.TFluid ->100,TEngineWallChamber]
Solve [localqPerKeyhot == - localconvectionQ/.TEngineWallInner->114/.TFluid ->100,TEngineWallChamber]
Solve [localqPerKeyhot == -localconvectionQ/.TEngineWallInner->115/.TFluid ->100,TEngineWallChamber]
Solve [localqPerKeyhot == -localconvectionQ/.TEngineWallInner->116/.TFluid ->100,TEngineWallChamber]
Solve [localqPerKeyhot == -localconvectionQ/.TEngineWallInner->117/.TFluid ->100,TEngineWallChamber]
Solve [localqPerKeyhot == -localconvectionQ/.TEngineWallInner->118/.TFluid ->100,TEngineWallChamber]
Solve [localqPerKeyhot == -localconvectionQ/.TEngineWallInner->119/.TFluid ->100,TEngineWallChamber]
Solve [localqPerKeyhot == -localconvectionQ/.TEngineWallInner->120/.TFluid ->100,TEngineWallChamber]
120
Solve [localqPerKeyhot == -localconvectionQ/.TEngineWallInner->121/.TFluid ->100,TEngineWallChamber]
121
Solve [localqPerKeyhot == -localconvectionQ/.TEngineWallInner->122/.TFluid ->100,TEngineWallChamber]
122
Solve [localqPerKeyhot == -localconvectionQ/.TEngineWallInner->123/.TFluid ->100,TEngineWallChamber]
123
Solve [localqPerKeyhot == -localconvectionQ/.TEngineWallInner->124/.TFluid ->100,TEngineWallChamber]
124:
Solve [localqPerKeyhot == -localconvectionQ/.TEngineWallInner->125/.TFluid ->100,TEngineWallChamber]
125:
Solve [localqPerKeyhot == -localconvectionQ/.TEngineWallInner->130/.TFluid ->100,TEngineWallChamber]
Solve [localqPerKeyhot == -localconvectionQ/.TEngineWallInner->135/.TFluid ->100,TEngineWallChamber]
Solve [localqPerKeyhot == -localconvectionQ/.TEngineWallInner->140/.TFluid ->100,TEngineWallChamber]*)

startup

Startup

 MaxMemoryUsed[ ] MemoryInUse[ ]

propulsion

results

[Graphics:HTMLFiles/xxrocket_heatfeb15_2004htmlized_395.gif]

RowBox[{ , RowBox[{ω =. ; radialelongation = . ; modulusElasticity =. ; <br / ... 371;, )}]}], ]}]}], , (* j *), , (*Print["foo "] ; *), , )}]}], ]}]}]}]

$RowBox[{stainlesssteel420, , thrust = , , 100, , chht , , 0.0119781, , vol in^3 = , , 0.329466}]$

rBot	Wall	stress lbf	sp thrust	weight	dia	dia ft	r max stress	min # noz	max # noz
0.00316228	0.000464159	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	146.447	0.682843	0.031209	0.103866	RowBox[{RowBox[{0.010485, }], +, RowBox[{0.010485, , i}]}]	0	0
0.00316228	0.000696238	RowBox[{RowBox[{119594., }], -, RowBox[{41364.4, , i}]}]	142.362	0.702436	0.0316732	0.105411	RowBox[{RowBox[{0.00763587, }], +, RowBox[{0.00763587, , i}]}]	0	0
0.00316228	0.000928318	88669.3	138.468	0.722188	0.0321374	0.106956	0.00811988	0	0
0.00316228	0.0011604	63939.7	134.754	0.742096	0.0326015	0.108501	0.0111735	0	0
0.00316228	0.00162456	44439.1	127.817	0.782369	0.0335298	0.11159	0.0131036	0	0
0.00316228	0.00185664	39416.1	124.575	0.802731	0.033994	0.113135	0.013609	0	0
0.00316228	0.00208871	35874.2	121.471	0.823239	0.0344582	0.11468	0.0139929	0	0
0.00316228	0.00232079	33313.	118.498	0.843893	0.0349223	0.116224	0.0143017	0	0
0.00316228	0.00255287	31439.5	115.649	0.864689	0.0353865	0.117769	0.0145604	0	0
0.00316228	0.00278495	30069.6	112.915	0.885625	0.0358506	0.119314	0.0147839	0	0
0.00316228	0.00301703	29080.9	110.29	0.906699	0.0363148	0.120859	0.0149817	0	0
0.00316228	0.00324911	28389.4	107.769	0.927909	0.036779	0.122403	0.0151602	0	0
0.00316228	0.00348119	27934.7	105.346	0.949253	0.0372431	0.123948	0.0153235	0	0
0.00316228	0.00371327	27672.9	103.015	0.970729	0.0377073	0.125493	0.015475	0	0
0.00316228	0.00394535	27570.9	100.773	0.992333	0.0381714	0.127038	0.0156169	0	0

$RowBox[{stainlesssteel420, , thrust = , , 1000, , chht , , 0.025806, , vol in^3 = , , 3.29466}]$

rBot	Wall	stress lbf	sp thrust	weight	dia	dia ft	r max stress	min # noz	max # noz
0.01	0.001	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	398.483	2.50952	0.073612	0.244987	RowBox[{RowBox[{0.0225893, }], +, RowBox[{0.0225893, , i}]}]	0	0
0.01	0.0015	RowBox[{RowBox[{119594., }], -, RowBox[{41364.4, , i}]}]	387.607	2.57993	0.074612	0.248315	RowBox[{RowBox[{0.016451, }], +, RowBox[{0.016451, , i}]}]	0	0
0.01	0.002	88669.3	377.308	2.65035	0.075612	0.251643	0.0174937	0	0
0.01	0.0025	63939.7	367.544	2.72077	0.076612	0.254971	0.0240726	0	0
0.01	0.0035	44439.1	349.472	2.86146	0.078612	0.261627	0.0282309	0	0
0.01	0.004	39416.1	341.099	2.9317	0.079612	0.264955	0.0293196	0	0
0.01	0.0045	35874.2	333.129	3.00184	0.080612	0.268284	0.0301468	0	0
0.01	0.005	33313.	325.536	3.07186	0.081612	0.271612	0.0308121	0	0
0.01	0.0055	31439.5	318.296	3.14173	0.082612	0.27494	0.0313694	0	0
0.01	0.006	30069.6	311.387	3.21143	0.083612	0.278268	0.031851	0	0
0.01	0.0065	29080.9	304.79	3.28095	0.084612	0.281596	0.0322772	0	0
0.01	0.007	28389.4	298.485	3.35025	0.085612	0.284924	0.0326616	0	0
0.01	0.0075	27934.7	292.456	3.41932	0.086612	0.288252	0.0330136	0	0
0.01	0.008	27672.9	286.687	3.48813	0.087612	0.29158	0.0333399	0	0
0.01	0.0085	27570.9	281.162	3.55666	0.088612	0.294908	0.0336455	0	0

$RowBox[{stainlesssteel420, , thrust = , , 3000, , chht , , 0.0372187, , vol in^3 = , , 9.88399}]$

rBot	Wall	stress lbf	sp thrust	weight	dia	dia ft	r max stress	min # noz	max # noz
0.0173205	0.00144225	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	778.633	3.85291	0.111963	0.372622	RowBox[{RowBox[{0.0325795, }], +, RowBox[{0.0325795, , i}]}]	0	0
0.0173205	0.00216337	RowBox[{RowBox[{119594., }], -, RowBox[{41364.4, , i}]}]	756.788	3.96412	0.113405	0.377422	RowBox[{RowBox[{0.0237264, }], +, RowBox[{0.0237264, , i}]}]	0	0
0.0173205	0.0028845	88669.3	736.356	4.07412	0.114847	0.382222	0.0252304	0	0
0.0173205	0.00360562	63939.7	717.219	4.18282	0.11629	0.387022	0.0347187	0	0
0.0173205	0.00504787	44439.1	682.422	4.3961	0.119174	0.396622	0.040716	0	0
0.0173205	0.005769	39416.1	666.586	4.50055	0.120616	0.401422	0.0422862	0	0
0.0173205	0.00649012	35874.2	651.688	4.60343	0.122059	0.406221	0.0434792	0	0
0.0173205	0.00721125	33313.	637.66	4.7047	0.123501	0.411021	0.0444387	0	0
0.0173205	0.00793237	31439.5	624.444	4.80428	0.124943	0.415821	0.0452425	0	0
0.0173205	0.0086535	30069.6	611.982	4.9021	0.126385	0.420621	0.0459371	0	0
0.0173205	0.00937462	29080.9	600.228	4.9981	0.127828	0.425421	0.0465518	0	0
0.0173205	0.0100957	28389.4	589.134	5.09222	0.12927	0.430221	0.0471061	0	0
0.0173205	0.0108169	27934.7	578.661	5.18438	0.130712	0.435021	0.0476138	0	0
0.0173205	0.011538	27672.9	568.772	5.27452	0.132154	0.439821	0.0480844	0	0
0.0173205	0.0122591	27570.9	559.432	5.36258	0.133597	0.444621	0.0485253	0	0

$RowBox[{stainlesssteel420, , thrust = , , 10000, , chht , , 0.0555973, , vol in^3 = , , 32.9466}]$

rBot	Wall	stress lbf	sp thrust	weight	dia	dia ft	r max stress	min # noz	max # noz
0.0316228	0.00215443	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	2881.	3.47101	0.178749	0.594892	RowBox[{RowBox[{0.0486673, }], +, RowBox[{0.0486673, , i}]}]	0	0
0.0316228	0.00323165	RowBox[{RowBox[{119594., }], -, RowBox[{41364.4, , i}]}]	2783.56	3.59252	0.180904	0.602062	RowBox[{RowBox[{0.0354426, }], +, RowBox[{0.0354426, , i}]}]	0	0
0.0316228	0.00430887	88669.3	2697.72	3.70684	0.183058	0.609232	0.0376891	0	0
0.0316228	0.00538609	63939.7	2622.1	3.81374	0.185212	0.616403	0.0518629	0	0
0.0316228	0.00754052	44439.1	2497.24	4.00442	0.189521	0.630743	0.0608217	0	0
0.0316228	0.00861774	39416.1	2446.33	4.08776	0.191676	0.637913	0.0631672	0	0
0.0316228	0.00969496	35874.2	2402.24	4.16279	0.19383	0.645083	0.0649493	0	0
0.0316228	0.0107722	33313.	2364.46	4.2293	0.195985	0.652253	0.0663826	0	0
0.0316228	0.0118494	31439.5	2332.6	4.28707	0.198139	0.659423	0.0675834	0	0
0.0316228	0.0129266	30069.6	2306.34	4.33587	0.200293	0.666593	0.0686209	0	0
0.0316228	0.0140038	29080.9	2285.46	4.37548	0.202448	0.673764	0.0695391	0	0
0.0316228	0.015081	28389.4	2269.79	4.40569	0.204602	0.680934	0.0703672	0	0
0.0316228	0.0161583	27934.7	2259.24	4.42626	0.206757	0.688104	0.0711255	0	0
0.0316228	0.0172355	27672.9	2253.79	4.43698	0.208911	0.695274	0.0718286	0	0
0.0316228	0.0183127	27570.9	2253.46	4.43762	0.211066	0.702444	0.0724871	0	0

$RowBox[{stainlesssteel420, , thrust = , , 50000, , chht , , 0.0950701, , vol in^3 = , , 164.733}]$

rBot	Wall	stress lbf	sp thrust	weight	dia	dia ft	r max stress	min # noz	max # noz
0.0416197	0.00368403	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	RowBox[{-, 2197.44}]	RowBox[{-, 22.7537}]	0.280748	0.934352	RowBox[{RowBox[{0.0832198, }], +, RowBox[{0.0832198, , i}]}]	0	0
0.0416197	0.00552605	RowBox[{RowBox[{119594., }], -, RowBox[{41364.4, , i}]}]	RowBox[{-, 2155.74}]	RowBox[{-, 23.1939}]	0.284432	0.946613	RowBox[{RowBox[{0.0606059, }], +, RowBox[{0.0606059, , i}]}]	0	0
0.0416197	0.00736806	88669.3	RowBox[{-, 2111.2}]	RowBox[{-, 23.6832}]	0.288116	0.958874	0.0644475	0	0
0.0416197	0.00921008	63939.7	RowBox[{-, 2064.19}]	RowBox[{-, 24.2226}]	0.2918	0.971135	0.0886843	0	0
0.0416197	0.0128941	44439.1	RowBox[{-, 1964.14}]	RowBox[{-, 25.4564}]	0.299168	0.995656	0.104004	0	0
0.0416197	0.0147361	39416.1	RowBox[{-, 1911.83}]	RowBox[{-, 26.153}]	0.302852	1.00792	0.108014	0	0
0.0416197	0.0165781	35874.2	RowBox[{-, 1858.45}]	RowBox[{-, 26.9042}]	0.306536	1.02018	0.111062	0	0
0.0416197	0.0184202	33313.	RowBox[{-, 1804.33}]	RowBox[{-, 27.7111}]	0.31022	1.03244	0.113513	0	0
0.0416197	0.0202622	31439.5	RowBox[{-, 1749.79}]	RowBox[{-, 28.5749}]	0.313904	1.0447	0.115566	0	0
0.0416197	0.0221042	30069.6	RowBox[{-, 1695.11}]	RowBox[{-, 29.4966}]	0.317588	1.05696	0.11734	0	0
0.0416197	0.0239462	29080.9	RowBox[{-, 1640.57}]	RowBox[{-, 30.4773}]	0.321272	1.06922	0.11891	0	0
0.0416197	0.0257882	28389.4	RowBox[{-, 1586.38}]	RowBox[{-, 31.5182}]	0.324956	1.08148	0.120326	0	0
0.0416197	0.0276302	27934.7	RowBox[{-, 1532.78}]	RowBox[{-, 32.6204}]	0.32864	1.09374	0.121623	0	0
0.0416197	0.0294723	27672.9	RowBox[{-, 1479.95}]	RowBox[{-, 33.7849}]	0.332324	1.106	0.122825	0	0
0.0416197	0.0313143	27570.9	RowBox[{-, 1428.04}]	RowBox[{-, 35.013}]	0.336008	1.11826	0.123951	0	0

$RowBox[{stainlesssteel420, , thrust = , , 100000, , chht , , 0.119781, , vol in^3 = , , 329.466}]$

rBot	Wall	stress lbf	sp thrust	weight	dia	dia ft	r max stress	min # noz	max # noz
0.05	0.00464159	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	RowBox[{-, 1448.04}]	RowBox[{-, 69.0591}]	0.348845	1.16099	RowBox[{RowBox[{0.10485, }], +, RowBox[{0.10485, , i}]}]	0	0
0.05	0.00696238	RowBox[{RowBox[{119594., }], -, RowBox[{41364.4, , i}]}]	RowBox[{-, 1417.47}]	RowBox[{-, 70.5483}]	0.353486	1.17643	RowBox[{RowBox[{0.0763587, }], +, RowBox[{0.0763587, , i}]}]	0	0
0.05	0.00928318	88669.3	RowBox[{-, 1386.13}]	RowBox[{-, 72.1433}]	0.358128	1.19188	0.0811988	0	0
0.05	0.011604	63939.7	RowBox[{-, 1354.16}]	RowBox[{-, 73.8463}]	0.36277	1.20733	0.111735	0	0
0.05	0.0162456	44439.1	RowBox[{-, 1288.91}]	RowBox[{-, 77.5849}]	0.372053	1.23822	0.131036	0	0
0.05	0.0185664	39416.1	RowBox[{-, 1255.89}]	RowBox[{-, 79.6251}]	0.376694	1.25367	0.13609	0	0
0.05	0.0208871	35874.2	RowBox[{-, 1222.76}]	RowBox[{-, 81.7821}]	0.381336	1.26912	0.139929	0	0
0.05	0.0232079	33313.	RowBox[{-, 1189.65}]	RowBox[{-, 84.0581}]	0.385978	1.28457	0.143017	0	0
0.05	0.0255287	31439.5	RowBox[{-, 1156.66}]	RowBox[{-, 86.4555}]	0.390619	1.30001	0.145604	0	0
0.05	0.0278495	30069.6	RowBox[{-, 1123.89}]	RowBox[{-, 88.9763}]	0.395261	1.31546	0.147839	0	0
0.05	0.0301703	29080.9	RowBox[{-, 1091.43}]	RowBox[{-, 91.6229}]	0.399902	1.33091	0.149817	0	0
0.05	0.0324911	28389.4	RowBox[{-, 1059.35}]	RowBox[{-, 94.3974}]	0.404544	1.34636	0.151602	0	0
0.05	0.0348119	27934.7	RowBox[{-, 1027.73}]	RowBox[{-, 97.302}]	0.409186	1.3618	0.153235	0	0
0.05	0.0371327	27672.9	RowBox[{-, 996.621}]	RowBox[{-, 100.339}]	0.413827	1.37725	0.15475	0	0
0.05	0.0394535	27570.9	RowBox[{-, 966.084}]	RowBox[{-, 103.511}]	0.418469	1.3927	0.156169	0	0

$RowBox[{stainlesssteel420, , thrust = , , 300000, , chht , , 0.172754, , vol in^3 = , , 988.399}]$

rBot	Wall	stress lbf	sp thrust	weight	dia	dia ft	r max stress	min # noz	max # noz
0.0699219	0.00669433	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	RowBox[{-, 1031.09}]	RowBox[{-, 290.953}]	0.49874	1.65985	RowBox[{RowBox[{0.15122, }], +, RowBox[{0.15122, , i}]}]	0	0
0.0699219	0.0100415	RowBox[{RowBox[{119594., }], -, RowBox[{41364.4, , i}]}]	RowBox[{-, 1008.15}]	RowBox[{-, 297.576}]	0.505435	1.68213	RowBox[{RowBox[{0.110128, }], +, RowBox[{0.110128, , i}]}]	0	0
0.0699219	0.0133887	88669.3	RowBox[{-, 985.085}]	RowBox[{-, 304.542}]	0.512129	1.70441	0.117109	0	0
0.0699219	0.0167358	63939.7	RowBox[{-, 961.97}]	RowBox[{-, 311.86}]	0.518823	1.72669	0.16115	0	0
0.0699219	0.0234302	44439.1	RowBox[{-, 915.822}]	RowBox[{-, 327.575}]	0.532212	1.77125	0.188987	0	0
0.0699219	0.0267773	39416.1	RowBox[{-, 892.897}]	RowBox[{-, 335.985}]	0.538906	1.79353	0.196275	0	0
0.0699219	0.0301245	35874.2	RowBox[{-, 870.139}]	RowBox[{-, 344.773}]	0.545601	1.8158	0.201813	0	0
0.0699219	0.0334716	33313.	RowBox[{-, 847.591}]	RowBox[{-, 353.944}]	0.552295	1.83808	0.206266	0	0
0.0699219	0.0368188	31439.5	RowBox[{-, 825.293}]	RowBox[{-, 363.507}]	0.558989	1.86036	0.209997	0	0
0.0699219	0.040166	30069.6	RowBox[{-, 803.283}]	RowBox[{-, 373.467}]	0.565684	1.88264	0.213221	0	0
0.0699219	0.0435131	29080.9	RowBox[{-, 781.593}]	RowBox[{-, 383.832}]	0.572378	1.90492	0.216074	0	0
0.0699219	0.0468603	28389.4	RowBox[{-, 760.251}]	RowBox[{-, 394.607}]	0.579072	1.9272	0.218647	0	0
0.0699219	0.0502075	27934.7	RowBox[{-, 739.282}]	RowBox[{-, 405.799}]	0.585767	1.94948	0.221004	0	0
0.0699219	0.0535546	27672.9	RowBox[{-, 718.708}]	RowBox[{-, 417.416}]	0.592461	1.97176	0.223188	0	0
0.0699219	0.0569018	27570.9	RowBox[{-, 698.547}]	RowBox[{-, 429.463}]	0.599155	1.99404	0.225234	0	0

$RowBox[{stainlesssteel420, , thrust = , , 500000, , chht , , 0.204822, , vol in^3 = , , 1647.33}]$

rBot	Wall	stress lbf	sp thrust	weight	dia	dia ft	r max stress	min # noz	max # noz
0.0828489	0.00793701	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	RowBox[{-, 935.393}]	RowBox[{-, 534.535}]	0.591217	1.96762	RowBox[{RowBox[{0.179292, }], +, RowBox[{0.179292, , i}]}]	0	0
0.0828489	0.0119055	RowBox[{RowBox[{119594., }], -, RowBox[{41364.4, , i}]}]	RowBox[{-, 914.338}]	RowBox[{-, 546.844}]	0.599154	1.99403	RowBox[{RowBox[{0.130571, }], +, RowBox[{0.130571, , i}]}]	0	0
0.0828489	0.015874	88669.3	RowBox[{-, 893.267}]	RowBox[{-, 559.743}]	0.607091	2.02045	0.138848	0	0
0.0828489	0.0198425	63939.7	RowBox[{-, 872.232}]	RowBox[{-, 573.242}]	0.615028	2.04686	0.191064	0	0
0.0828489	0.0277795	44439.1	RowBox[{-, 830.444}]	RowBox[{-, 602.088}]	0.630902	2.09969	0.224069	0	0
0.0828489	0.031748	39416.1	RowBox[{-, 809.775}]	RowBox[{-, 617.456}]	0.638839	2.12611	0.23271	0	0
0.0828489	0.0357165	35874.2	RowBox[{-, 789.305}]	RowBox[{-, 633.469}]	0.646776	2.15252	0.239275	0	0
0.0828489	0.039685	33313.	RowBox[{-, 769.067}]	RowBox[{-, 650.138}]	0.654713	2.17894	0.244556	0	0
0.0828489	0.0436535	31439.5	RowBox[{-, 749.092}]	RowBox[{-, 667.475}]	0.66265	2.20535	0.248979	0	0
0.0828489	0.047622	30069.6	RowBox[{-, 729.406}]	RowBox[{-, 685.49}]	0.670587	2.23177	0.252802	0	0
0.0828489	0.0515905	29080.9	RowBox[{-, 710.032}]	RowBox[{-, 704.194}]	0.678524	2.25818	0.256184	0	0
0.0828489	0.055559	28389.4	RowBox[{-, 690.991}]	RowBox[{-, 723.599}]	0.686461	2.2846	0.259235	0	0
0.0828489	0.0595275	27934.7	RowBox[{-, 672.3}]	RowBox[{-, 743.715}]	0.694398	2.31101	0.262029	0	0
0.0828489	0.063496	27672.9	RowBox[{-, 653.975}]	RowBox[{-, 764.555}]	0.702335	2.33743	0.264619	0	0
0.0828489	0.0674645	27570.9	RowBox[{-, 636.029}]	RowBox[{-, 786.128}]	0.710272	2.36384	0.267045	0	0

$RowBox[{stainlesssteel420, , thrust = , , 1000000, , chht , , 0.25806, , vol in^3 = , , 3294.66}]$

rBot	Wall	stress lbf	sp thrust	weight	dia	dia ft	r max stress	min # noz	max # noz
0.105409	0.01	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	RowBox[{-, 847.768}]	RowBox[{-, 1179.57}]	0.746939	2.48587	RowBox[{RowBox[{0.225893, }], +, RowBox[{0.225893, , i}]}]	0	0
0.105409	0.015	RowBox[{RowBox[{119594., }], -, RowBox[{41364.4, , i}]}]	RowBox[{-, 828.492}]	RowBox[{-, 1207.01}]	0.756939	2.51916	RowBox[{RowBox[{0.16451, }], +, RowBox[{0.16451, , i}]}]	0	0
0.105409	0.02	88669.3	RowBox[{-, 809.277}]	RowBox[{-, 1235.67}]	0.766939	2.55244	0.174937	0	0
0.105409	0.025	63939.7	RowBox[{-, 790.16}]	RowBox[{-, 1265.57}]	0.776939	2.58572	0.240726	0	0
0.105409	0.035	44439.1	RowBox[{-, 752.356}]	RowBox[{-, 1329.16}]	0.796939	2.65228	0.282309	0	0
0.105409	0.04	39416.1	RowBox[{-, 733.731}]	RowBox[{-, 1362.9}]	0.806939	2.68556	0.293196	0	0
0.105409	0.045	35874.2	RowBox[{-, 715.327}]	RowBox[{-, 1397.96}]	0.816939	2.71884	0.301468	0	0
0.105409	0.05	33313.	RowBox[{-, 697.168}]	RowBox[{-, 1434.37}]	0.826939	2.75212	0.308121	0	0
0.105409	0.055	31439.5	RowBox[{-, 679.276}]	RowBox[{-, 1472.16}]	0.836939	2.7854	0.313694	0	0
0.105409	0.06	30069.6	RowBox[{-, 661.669}]	RowBox[{-, 1511.33}]	0.846939	2.81868	0.31851	0	0
0.105409	0.065	29080.9	RowBox[{-, 644.364}]	RowBox[{-, 1551.92}]	0.856939	2.85196	0.322772	0	0
0.105409	0.07	28389.4	RowBox[{-, 627.375}]	RowBox[{-, 1593.94}]	0.866939	2.88524	0.326616	0	0
0.105409	0.075	27934.7	RowBox[{-, 610.714}]	RowBox[{-, 1637.43}]	0.876939	2.91853	0.330136	0	0
0.105409	0.08	27672.9	RowBox[{-, 594.392}]	RowBox[{-, 1682.39}]	0.886939	2.95181	0.333399	0	0
0.105409	0.085	27570.9	RowBox[{-, 578.416}]	RowBox[{-, 1728.86}]	0.896939	2.98509	0.336455	0	0

$RowBox[{stainlesssteel420, , thrust = , , 1500000, , chht , , 0.295405, , vol in^3 = , , 4942.}]$

rBot	Wall	stress lbf	sp thrust	weight	dia	dia ft	r max stress	min # noz	max # noz
0.121942	0.0114471	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	RowBox[{-, 810.769}]	RowBox[{-, 1850.09}]	0.857588	2.85412	RowBox[{RowBox[{0.258583, }], +, RowBox[{0.258583, , i}]}]	0	0
0.121942	0.0171707	RowBox[{RowBox[{119594., }], -, RowBox[{41364.4, , i}]}]	RowBox[{-, 792.258}]	RowBox[{-, 1893.32}]	0.869035	2.89222	RowBox[{RowBox[{0.188317, }], +, RowBox[{0.188317, , i}]}]	0	0
0.121942	0.0228943	88669.3	RowBox[{-, 773.834}]	RowBox[{-, 1938.4}]	0.880482	2.93032	0.200253	0	0
0.121942	0.0286179	63939.7	RowBox[{-, 755.532}]	RowBox[{-, 1985.36}]	0.891929	2.96842	0.275563	0	0
0.121942	0.040065	44439.1	RowBox[{-, 719.408}]	RowBox[{-, 2085.05}]	0.914824	3.04461	0.323163	0	0
0.121942	0.0457886	39416.1	RowBox[{-, 701.641}]	RowBox[{-, 2137.85}]	0.926271	3.08271	0.335626	0	0
0.121942	0.0515121	35874.2	RowBox[{-, 684.101}]	RowBox[{-, 2192.66}]	0.937718	3.1208	0.345095	0	0
0.121942	0.0572357	33313.	RowBox[{-, 666.809}]	RowBox[{-, 2249.52}]	0.949165	3.1589	0.35271	0	0
0.121942	0.0629593	31439.5	RowBox[{-, 649.783}]	RowBox[{-, 2308.46}]	0.960612	3.197	0.35909	0	0
0.121942	0.0686829	30069.6	RowBox[{-, 633.04}]	RowBox[{-, 2369.52}]	0.972059	3.2351	0.364603	0	0
0.121942	0.0744064	29080.9	RowBox[{-, 616.594}]	RowBox[{-, 2432.72}]	0.983506	3.27319	0.369482	0	0
0.121942	0.08013	28389.4	RowBox[{-, 600.455}]	RowBox[{-, 2498.1}]	0.994954	3.31129	0.373882	0	0
0.121942	0.0858536	27934.7	RowBox[{-, 584.636}]	RowBox[{-, 2565.7}]	1.0064	3.34939	0.377911	0	0
0.121942	0.0915771	27672.9	RowBox[{-, 569.142}]	RowBox[{-, 2635.54}]	1.01785	3.38748	0.381647	0	0
0.121942	0.0973007	27570.9	RowBox[{-, 553.982}]	RowBox[{-, 2707.67}]	1.0293	3.42558	0.385145	0	0

$RowBox[{stainlesssteel420, , thrust = , , 2000000, , chht , , 0.325135, , vol in^3 = , , 6589.33}]$

rBot	Wall	stress lbf	sp thrust	weight	dia	dia ft	r max stress	min # noz	max # noz
0.135477	0.0125992	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	RowBox[{-, 788.994}]	RowBox[{-, 2534.87}]	0.946423	3.14978	RowBox[{RowBox[{0.284608, }], +, RowBox[{0.284608, , i}]}]	0	0
0.135477	0.0188988	RowBox[{RowBox[{119594., }], -, RowBox[{41364.4, , i}]}]	RowBox[{-, 770.936}]	RowBox[{-, 2594.25}]	0.959022	3.19171	RowBox[{RowBox[{0.207269, }], +, RowBox[{0.207269, , i}]}]	0	0
0.135477	0.0251984	88669.3	RowBox[{-, 752.981}]	RowBox[{-, 2656.11}]	0.971621	3.23364	0.220407	0	0
0.135477	0.031498	63939.7	RowBox[{-, 735.159}]	RowBox[{-, 2720.5}]	0.984221	3.27557	0.303296	0	0
0.135477	0.0440972	44439.1	RowBox[{-, 700.023}]	RowBox[{-, 2857.05}]	1.00942	3.35943	0.355687	0	0
0.135477	0.0503968	39416.1	RowBox[{-, 682.759}]	RowBox[{-, 2929.29}]	1.02202	3.40136	0.369404	0	0
0.135477	0.0566964	35874.2	RowBox[{-, 665.725}]	RowBox[{-, 3004.25}]	1.03462	3.44329	0.379826	0	0
0.135477	0.0629961	33313.	RowBox[{-, 648.94}]	RowBox[{-, 3081.95}]	1.04722	3.48522	0.388208	0	0
0.135477	0.0692957	31439.5	RowBox[{-, 632.421}]	RowBox[{-, 3162.45}]	1.05982	3.52716	0.39523	0	0
0.135477	0.0755953	30069.6	RowBox[{-, 616.183}]	RowBox[{-, 3245.79}]	1.07242	3.56909	0.401298	0	0
0.135477	0.0818949	29080.9	RowBox[{-, 600.238}]	RowBox[{-, 3332.01}]	1.08501	3.61102	0.406667	0	0
0.135477	0.0881945	28389.4	RowBox[{-, 584.596}]	RowBox[{-, 3421.17}]	1.09761	3.65295	0.41151	0	0
0.135477	0.0944941	27934.7	RowBox[{-, 569.266}]	RowBox[{-, 3513.29}]	1.11021	3.69488	0.415945	0	0
0.135477	0.100794	27672.9	RowBox[{-, 554.256}]	RowBox[{-, 3608.44}]	1.12281	3.73681	0.420056	0	0
0.135477	0.107093	27570.9	RowBox[{-, 539.572}]	RowBox[{-, 3706.64}]	1.13541	3.77874	0.423907	0	0

$RowBox[{stainlesssteel420, , thrust = , , 3000000, , chht , , 0.372187, , vol in^3 = , , 9883.99}]$

rBot	Wall	stress lbf	sp thrust	weight	dia	dia ft	r max stress	min # noz	max # noz
0.157522	0.0144225	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	RowBox[{-, 763.225}]	RowBox[{-, 3930.69}]	1.08826	3.62183	RowBox[{RowBox[{0.325795, }], +, RowBox[{0.325795, , i}]}]	0	0
0.157522	0.0216337	RowBox[{RowBox[{119594., }], -, RowBox[{41364.4, , i}]}]	RowBox[{-, 745.708}]	RowBox[{-, 4023.02}]	1.10269	3.66983	RowBox[{RowBox[{0.237264, }], +, RowBox[{0.237264, , i}]}]	0	0
0.157522	0.028845	88669.3	RowBox[{-, 728.31}]	RowBox[{-, 4119.13}]	1.11711	3.71783	0.252304	0	0
0.157522	0.0360562	63939.7	RowBox[{-, 711.058}]	RowBox[{-, 4219.07}]	1.13153	3.76583	0.347187	0	0
0.157522	0.0504787	44439.1	RowBox[{-, 677.091}]	RowBox[{-, 4430.72}]	1.16038	3.86183	0.40716	0	0
0.157522	0.05769	39416.1	RowBox[{-, 660.42}]	RowBox[{-, 4542.57}]	1.1748	3.90983	0.422862	0	0
0.157522	0.0649012	35874.2	RowBox[{-, 643.982}]	RowBox[{-, 4658.51}]	1.18922	3.95782	0.434792	0	0
0.157522	0.0721125	33313.	RowBox[{-, 627.795}]	RowBox[{-, 4778.63}]	1.20364	4.00582	0.444387	0	0
0.157522	0.0793237	31439.5	RowBox[{-, 611.873}]	RowBox[{-, 4902.98}]	1.21807	4.05382	0.452425	0	0
0.157522	0.086535	30069.6	RowBox[{-, 596.228}]	RowBox[{-, 5031.63}]	1.23249	4.10182	0.459371	0	0
0.157522	0.0937462	29080.9	RowBox[{-, 580.872}]	RowBox[{-, 5164.65}]	1.24691	4.14982	0.465518	0	0
0.157522	0.100957	28389.4	RowBox[{-, 565.813}]	RowBox[{-, 5302.1}]	1.26133	4.19782	0.471061	0	0
0.157522	0.108169	27934.7	RowBox[{-, 551.06}]	RowBox[{-, 5444.06}]	1.27576	4.24582	0.476138	0	0
0.157522	0.11538	27672.9	RowBox[{-, 536.617}]	RowBox[{-, 5590.58}]	1.29018	4.29382	0.480844	0	0
0.157522	0.122591	27570.9	RowBox[{-, 522.49}]	RowBox[{-, 5741.74}]	1.3046	4.34182	0.485253	0	0

$RowBox[{stainlesssteel420, , thrust = , , 5000000, , chht , , 0.441276, , vol in^3 = , , 16473.3}]$

rBot	Wall	stress lbf	sp thrust	weight	dia	dia ft	r max stress	min # noz	max # noz
0.191163	0.0170998	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	RowBox[{-, 737.156}]	RowBox[{-, 6782.82}]	1.29908	4.32344	RowBox[{RowBox[{0.386272, }], +, RowBox[{0.386272, , i}]}]	0	0
0.191163	0.0256496	RowBox[{RowBox[{119594., }], -, RowBox[{41364.4, , i}]}]	RowBox[{-, 720.189}]	RowBox[{-, 6942.62}]	1.31618	4.38035	RowBox[{RowBox[{0.281308, }], +, RowBox[{0.281308, , i}]}]	0	0
0.191163	0.0341995	88669.3	RowBox[{-, 703.357}]	RowBox[{-, 7108.77}]	1.33328	4.43726	0.299139	0	0
0.191163	0.0427494	63939.7	RowBox[{-, 686.682}]	RowBox[{-, 7281.39}]	1.35038	4.49417	0.411636	0	0
0.191163	0.0598492	44439.1	RowBox[{-, 653.897}]	RowBox[{-, 7646.46}]	1.38458	4.60799	0.482742	0	0
0.191163	0.068399	39416.1	RowBox[{-, 637.825}]	RowBox[{-, 7839.14}]	1.40168	4.6649	0.501358	0	0
0.191163	0.0769489	35874.2	RowBox[{-, 621.989}]	RowBox[{-, 8038.73}]	1.41878	4.72181	0.515503	0	0
0.191163	0.0854988	33313.	RowBox[{-, 606.403}]	RowBox[{-, 8245.34}]	1.43588	4.77872	0.526879	0	0
0.191163	0.0940487	31439.5	RowBox[{-, 591.08}]	RowBox[{-, 8459.09}]	1.45298	4.83563	0.53641	0	0
0.191163	0.102599	30069.6	RowBox[{-, 576.032}]	RowBox[{-, 8680.07}]	1.47008	4.89254	0.544645	0	0
0.191163	0.111148	29080.9	RowBox[{-, 561.267}]	RowBox[{-, 8908.41}]	1.48718	4.94945	0.551932	0	0
0.191163	0.119698	28389.4	RowBox[{-, 546.794}]	RowBox[{-, 9144.21}]	1.50428	5.00636	0.558505	0	0
0.191163	0.128248	27934.7	RowBox[{-, 532.618}]	RowBox[{-, 9387.59}]	1.52138	5.06327	0.564524	0	0
0.191163	0.136798	27672.9	RowBox[{-, 518.744}]	RowBox[{-, 9638.66}]	1.53848	5.12018	0.570104	0	0
0.191163	0.145348	27570.9	RowBox[{-, 505.177}]	RowBox[{-, 9897.52}]	1.55558	5.17708	0.575331	0	0

$RowBox[{aluminum, , thrust = , , 100, , chht , , 0.0119781, , vol in^3 = , , 0.329466}]$

rBot	Wall	stress lbf	sp thrust	weight	dia	dia ft	r max stress	min # noz	max # noz
0.00316228	0.000464159	RowBox[{RowBox[{81647.1, }], -, RowBox[{60106.6, , i}]}]	405.343	0.246705	0.031209	0.103866	RowBox[{RowBox[{0.0153136, }], +, RowBox[{0.0153136, , i}]}]	0	0
0.00316228	0.000696238	RowBox[{RowBox[{63883.4, }], -, RowBox[{45488.4, , i}]}]	394.037	0.253784	0.0316732	0.105411	RowBox[{RowBox[{0.0133219, }], +, RowBox[{0.0133219, , i}]}]	0	0
0.00316228	0.000928318	RowBox[{RowBox[{55358.5, }], -, RowBox[{35912.7, , i}]}]	383.26	0.26092	0.0321374	0.106956	RowBox[{RowBox[{0.011837, }], +, RowBox[{0.011837, , i}]}]	0	0
0.00316228	0.0011604	RowBox[{RowBox[{50527.3, }], -, RowBox[{28557.6, , i}]}]	372.979	0.268112	0.0326015	0.108501	RowBox[{RowBox[{0.0105555, }], +, RowBox[{0.0105555, , i}]}]	0	0
0.00316228	0.00162456	RowBox[{RowBox[{45611.9, }], -, RowBox[{16084.8, , i}]}]	353.779	0.282662	0.0335298	0.11159	RowBox[{RowBox[{0.00792182, }], +, RowBox[{0.00792182, , i}]}]	0	0
0.00316228	0.00185664	RowBox[{RowBox[{44340.9, }], -, RowBox[{8821.6, , i}]}]	344.805	0.290019	0.033994	0.113135	RowBox[{RowBox[{0.00586666, }], +, RowBox[{0.00586666, , i}]}]	0	0
0.00316228	0.00208871	35313.5	336.215	0.297428	0.0344582	0.11468	0.00799721	0	0
0.00316228	0.00232079	29305.8	327.987	0.30489	0.0349223	0.116224	0.0103323	0	0
0.00316228	0.00255287	25686.	320.099	0.312404	0.0353865	0.117769	0.0115186	0	0
0.00316228	0.00278495	23129.1	312.532	0.319968	0.0358506	0.119314	0.0123137	0	0
0.00316228	0.00301703	21213.6	305.267	0.327582	0.0363148	0.120859	0.0129072	0	0
0.00316228	0.00324911	19733.8	298.29	0.335245	0.036779	0.122403	0.0133781	0	0
0.00316228	0.00348119	18570.	291.583	0.342956	0.0372431	0.123948	0.0137674	0	0
0.00316228	0.00371327	17645.9	285.132	0.350715	0.0377073	0.125493	0.0140987	0	0
0.00316228	0.00394535	16909.1	278.924	0.35852	0.0381714	0.127038	0.0143873	0	0

$RowBox[{aluminum, , thrust = , , 1000, , chht , , 0.025806, , vol in^3 = , , 3.29466}]$

rBot	Wall	stress lbf	sp thrust	weight	dia	dia ft	r max stress	min # noz	max # noz
0.01	0.001	RowBox[{RowBox[{81647.1, }], -, RowBox[{60106.6, , i}]}]	1102.94	0.906665	0.073612	0.244987	RowBox[{RowBox[{0.0329922, }], +, RowBox[{0.0329922, , i}]}]	0	0
0.01	0.0015	RowBox[{RowBox[{63883.4, }], -, RowBox[{45488.4, , i}]}]	1072.84	0.932104	0.074612	0.248315	RowBox[{RowBox[{0.0287012, }], +, RowBox[{0.0287012, , i}]}]	0	0
0.01	0.002	RowBox[{RowBox[{55358.5, }], -, RowBox[{35912.7, , i}]}]	1044.33	0.957547	0.075612	0.251643	RowBox[{RowBox[{0.025502, }], +, RowBox[{0.025502, , i}]}]	0	0
0.01	0.0025	RowBox[{RowBox[{50527.3, }], -, RowBox[{28557.6, , i}]}]	1017.31	0.982986	0.076612	0.254971	RowBox[{RowBox[{0.0227411, }], +, RowBox[{0.0227411, , i}]}]	0	0
0.01	0.0035	RowBox[{RowBox[{45611.9, }], -, RowBox[{16084.8, , i}]}]	967.288	1.03382	0.078612	0.261627	RowBox[{RowBox[{0.0170671, }], +, RowBox[{0.0170671, , i}]}]	0	0
0.01	0.004	RowBox[{RowBox[{44340.9, }], -, RowBox[{8821.6, , i}]}]	944.113	1.0592	0.079612	0.264955	RowBox[{RowBox[{0.0126393, }], +, RowBox[{0.0126393, , i}]}]	0	0
0.01	0.0045	35313.5	922.053	1.08454	0.080612	0.268284	0.0172295	0	0
0.01	0.005	29305.8	901.036	1.10983	0.081612	0.271612	0.0222602	0	0
0.01	0.0055	25686.	880.998	1.13508	0.082612	0.27494	0.024816	0	0
0.01	0.006	23129.1	861.876	1.16026	0.083612	0.278268	0.0265291	0	0
0.01	0.0065	21213.6	843.615	1.18537	0.084612	0.281596	0.0278078	0	0
0.01	0.007	19733.8	826.164	1.21041	0.085612	0.284924	0.0288223	0	0
0.01	0.0075	18570.	809.476	1.23537	0.086612	0.288252	0.0296609	0	0
0.01	0.008	17645.9	793.507	1.26023	0.087612	0.29158	0.0303747	0	0
0.01	0.0085	16909.1	778.217	1.28499	0.088612	0.294908	0.0309964	0	0

$RowBox[{aluminum, , thrust = , , 10000, , chht , , 0.0555973, , vol in^3 = , , 32.9466}]$

rBot	Wall	stress lbf	sp thrust	weight	dia	dia ft	r max stress	min # noz	max # noz
0.0316228	0.00215443	RowBox[{RowBox[{81647.1, }], -, RowBox[{60106.6, , i}]}]	7974.2	1.25404	0.178749	0.594892	RowBox[{RowBox[{0.0710795, }], +, RowBox[{0.0710795, , i}]}]	0	0
0.0316228	0.00323165	RowBox[{RowBox[{63883.4, }], -, RowBox[{45488.4, , i}]}]	7704.5	1.29794	0.180904	0.602062	RowBox[{RowBox[{0.0618349, }], +, RowBox[{0.0618349, , i}]}]	0	0
0.0316228	0.00430887	RowBox[{RowBox[{55358.5, }], -, RowBox[{35912.7, , i}]}]	7466.89	1.33924	0.183058	0.609232	RowBox[{RowBox[{0.0549424, }], +, RowBox[{0.0549424, , i}]}]	0	0
0.0316228	0.00538609	RowBox[{RowBox[{50527.3, }], -, RowBox[{28557.6, , i}]}]	7257.59	1.37787	0.185212	0.616403	RowBox[{RowBox[{0.0489942, }], +, RowBox[{0.0489942, , i}]}]	0	0
0.0316228	0.00754052	RowBox[{RowBox[{45611.9, }], -, RowBox[{16084.8, , i}]}]	6912.	1.44676	0.189521	0.630743	RowBox[{RowBox[{0.0367698, }], +, RowBox[{0.0367698, , i}]}]	0	0
0.0316228	0.00861774	RowBox[{RowBox[{44340.9, }], -, RowBox[{8821.6, , i}]}]	6771.09	1.47687	0.191676	0.637913	RowBox[{RowBox[{0.0272306, }], +, RowBox[{0.0272306, , i}]}]	0	0
0.0316228	0.00969496	35313.5	6649.04	1.50398	0.19383	0.645083	0.0371198	0	0
0.0316228	0.0107722	29305.8	6544.48	1.52801	0.195985	0.652253	0.0479581	0	0
0.0316228	0.0118494	25686.	6456.29	1.54888	0.198139	0.659423	0.0534645	0	0
0.0316228	0.0129266	23129.1	6383.63	1.56651	0.200293	0.666593	0.0571553	0	0
0.0316228	0.0140038	21213.6	6325.83	1.58082	0.202448	0.673764	0.05991	0	0
0.0316228	0.015081	19733.8	6282.47	1.59173	0.204602	0.680934	0.0620958	0	0
0.0316228	0.0161583	18570.	6253.27	1.59916	0.206757	0.688104	0.0639024	0	0
0.0316228	0.0172355	17645.9	6238.16	1.60304	0.208911	0.695274	0.0654404	0	0
0.0316228	0.0183127	16909.1	6237.26	1.60327	0.211066	0.702444	0.0667798	0	0

$RowBox[{aluminum, , thrust = , , 50000, , chht , , 0.0950701, , vol in^3 = , , 164.733}]$

rBot	Wall	stress lbf	sp thrust	weight	dia	dia ft	r max stress	min # noz	max # noz
0.0416197	0.00368403	RowBox[{RowBox[{81647.1, }], -, RowBox[{60106.6, , i}]}]	RowBox[{-, 6082.2}]	RowBox[{-, 8.22071}]	0.280748	0.934352	RowBox[{RowBox[{0.121544, }], +, RowBox[{0.121544, , i}]}]	0	0
0.0416197	0.00552605	RowBox[{RowBox[{63883.4, }], -, RowBox[{45488.4, , i}]}]	RowBox[{-, 5966.77}]	RowBox[{-, 8.37974}]	0.284432	0.946613	RowBox[{RowBox[{0.105736, }], +, RowBox[{0.105736, , i}]}]	0	0
0.0416197	0.00736806	RowBox[{RowBox[{55358.5, }], -, RowBox[{35912.7, , i}]}]	RowBox[{-, 5843.51}]	RowBox[{-, 8.5565}]	0.288116	0.958874	RowBox[{RowBox[{0.0939502, }], +, RowBox[{0.0939502, , i}]}]	0	0
0.0416197	0.00921008	RowBox[{RowBox[{50527.3, }], -, RowBox[{28557.6, , i}]}]	RowBox[{-, 5713.38}]	RowBox[{-, 8.75138}]	0.2918	0.971135	RowBox[{RowBox[{0.0837788, }], +, RowBox[{0.0837788, , i}]}]	0	0
0.0416197	0.0128941	RowBox[{RowBox[{45611.9, }], -, RowBox[{16084.8, , i}]}]	RowBox[{-, 5436.47}]	RowBox[{-, 9.19714}]	0.299168	0.995656	RowBox[{RowBox[{0.0628756, }], +, RowBox[{0.0628756, , i}]}]	0	0
0.0416197	0.0147361	RowBox[{RowBox[{44340.9, }], -, RowBox[{8821.6, , i}]}]	RowBox[{-, 5291.67}]	RowBox[{-, 9.44881}]	0.302852	1.00792	RowBox[{RowBox[{0.0465637, }], +, RowBox[{0.0465637, , i}]}]	0	0
0.0416197	0.0165781	35313.5	RowBox[{-, 5143.92}]	RowBox[{-, 9.72022}]	0.306536	1.02018	0.0634739	0	0
0.0416197	0.0184202	29305.8	RowBox[{-, 4994.13}]	RowBox[{-, 10.0118}]	0.31022	1.03244	0.0820072	0	0
0.0416197	0.0202622	25686.	RowBox[{-, 4843.17}]	RowBox[{-, 10.3238}]	0.313904	1.0447	0.0914229	0	0
0.0416197	0.0221042	23129.1	RowBox[{-, 4691.83}]	RowBox[{-, 10.6568}]	0.317588	1.05696	0.0977341	0	0
0.0416197	0.0239462	21213.6	RowBox[{-, 4540.85}]	RowBox[{-, 11.0112}]	0.321272	1.06922	0.102445	0	0
0.0416197	0.0257882	19733.8	RowBox[{-, 4390.89}]	RowBox[{-, 11.3872}]	0.324956	1.08148	0.106182	0	0
0.0416197	0.0276302	18570.	RowBox[{-, 4242.53}]	RowBox[{-, 11.7854}]	0.32864	1.09374	0.109272	0	0
0.0416197	0.0294723	17645.9	RowBox[{-, 4096.29}]	RowBox[{-, 12.2062}]	0.332324	1.106	0.111902	0	0
0.0416197	0.0313143	16909.1	RowBox[{-, 3952.62}]	RowBox[{-, 12.6498}]	0.336008	1.11826	0.114192	0	0

$RowBox[{aluminum, , thrust = , , 100000, , chht , , 0.119781, , vol in^3 = , , 329.466}]$

rBot	Wall	stress lbf	sp thrust	weight	dia	dia ft	r max stress	min # noz	max # noz
0.05	0.00464159	RowBox[{RowBox[{81647.1, }], -, RowBox[{60106.6, , i}]}]	RowBox[{-, 4007.95}]	RowBox[{-, 24.9504}]	0.348845	1.16099	RowBox[{RowBox[{0.153136, }], +, RowBox[{0.153136, , i}]}]	0	0
0.05	0.00696238	RowBox[{RowBox[{63883.4, }], -, RowBox[{45488.4, , i}]}]	RowBox[{-, 3923.35}]	RowBox[{-, 25.4884}]	0.353486	1.17643	RowBox[{RowBox[{0.133219, }], +, RowBox[{0.133219, , i}]}]	0	0
0.05	0.00928318	RowBox[{RowBox[{55358.5, }], -, RowBox[{35912.7, , i}]}]	RowBox[{-, 3836.61}]	RowBox[{-, 26.0647}]	0.358128	1.19188	RowBox[{RowBox[{0.11837, }], +, RowBox[{0.11837, , i}]}]	0	0
0.05	0.011604	RowBox[{RowBox[{50527.3, }], -, RowBox[{28557.6, , i}]}]	RowBox[{-, 3748.13}]	RowBox[{-, 26.6799}]	0.36277	1.20733	RowBox[{RowBox[{0.105555, }], +, RowBox[{0.105555, , i}]}]	0	0
0.05	0.0162456	RowBox[{RowBox[{45611.9, }], -, RowBox[{16084.8, , i}]}]	RowBox[{-, 3567.52}]	RowBox[{-, 28.0307}]	0.372053	1.23822	RowBox[{RowBox[{0.0792182, }], +, RowBox[{0.0792182, , i}]}]	0	0
0.05	0.0185664	RowBox[{RowBox[{44340.9, }], -, RowBox[{8821.6, , i}]}]	RowBox[{-, 3476.11}]	RowBox[{-, 28.7678}]	0.376694	1.25367	RowBox[{RowBox[{0.0586666, }], +, RowBox[{0.0586666, , i}]}]	0	0
0.05	0.0208871	35313.5	RowBox[{-, 3384.43}]	RowBox[{-, 29.5471}]	0.381336	1.26912	0.0799721	0	0
0.05	0.0232079	29305.8	RowBox[{-, 3292.79}]	RowBox[{-, 30.3694}]	0.385978	1.28457	0.103323	0	0
0.05	0.0255287	25686.	RowBox[{-, 3201.48}]	RowBox[{-, 31.2355}]	0.390619	1.30001	0.115186	0	0
0.05	0.0278495	23129.1	RowBox[{-, 3110.78}]	RowBox[{-, 32.1463}]	0.395261	1.31546	0.123137	0	0
0.05	0.0301703	21213.6	RowBox[{-, 3020.92}]	RowBox[{-, 33.1025}]	0.399902	1.33091	0.129072	0	0
0.05	0.0324911	19733.8	RowBox[{-, 2932.13}]	RowBox[{-, 34.1049}]	0.404544	1.34636	0.133781	0	0
0.05	0.0348119	18570.	RowBox[{-, 2844.6}]	RowBox[{-, 35.1543}]	0.409186	1.3618	0.137674	0	0
0.05	0.0371327	17645.9	RowBox[{-, 2758.5}]	RowBox[{-, 36.2515}]	0.413827	1.37725	0.140987	0	0
0.05	0.0394535	16909.1	RowBox[{-, 2673.98}]	RowBox[{-, 37.3974}]	0.418469	1.3927	0.143873	0	0

$RowBox[{aluminum, , thrust = , , 300000, , chht , , 0.172754, , vol in^3 = , , 988.399}]$

rBot	Wall	stress lbf	sp thrust	weight	dia	dia ft	r max stress	min # noz	max # noz
0.0699219	0.00669433	RowBox[{RowBox[{81647.1, }], -, RowBox[{60106.6, , i}]}]	RowBox[{-, 2853.92}]	RowBox[{-, 105.118}]	0.49874	1.65985	RowBox[{RowBox[{0.220861, }], +, RowBox[{0.220861, , i}]}]	0	0
0.0699219	0.0100415	RowBox[{RowBox[{63883.4, }], -, RowBox[{45488.4, , i}]}]	RowBox[{-, 2790.41}]	RowBox[{-, 107.511}]	0.505435	1.68213	RowBox[{RowBox[{0.192136, }], +, RowBox[{0.192136, , i}]}]	0	0
0.0699219	0.0133887	RowBox[{RowBox[{55358.5, }], -, RowBox[{35912.7, , i}]}]	RowBox[{-, 2726.57}]	RowBox[{-, 110.028}]	0.512129	1.70441	RowBox[{RowBox[{0.170719, }], +, RowBox[{0.170719, , i}]}]	0	0
0.0699219	0.0167358	RowBox[{RowBox[{50527.3, }], -, RowBox[{28557.6, , i}]}]	RowBox[{-, 2662.6}]	RowBox[{-, 112.672}]	0.518823	1.72669	RowBox[{RowBox[{0.152236, }], +, RowBox[{0.152236, , i}]}]	0	0
0.0699219	0.0234302	RowBox[{RowBox[{45611.9, }], -, RowBox[{16084.8, , i}]}]	RowBox[{-, 2534.86}]	RowBox[{-, 118.35}]	0.532212	1.77125	RowBox[{RowBox[{0.114252, }], +, RowBox[{0.114252, , i}]}]	0	0
0.0699219	0.0267773	RowBox[{RowBox[{44340.9, }], -, RowBox[{8821.6, , i}]}]	RowBox[{-, 2471.41}]	RowBox[{-, 121.388}]	0.538906	1.79353	RowBox[{RowBox[{0.0846118, }], +, RowBox[{0.0846118, , i}]}]	0	0
0.0699219	0.0301245	35313.5	RowBox[{-, 2408.42}]	RowBox[{-, 124.563}]	0.545601	1.8158	0.11534	0	0
0.0699219	0.0334716	29305.8	RowBox[{-, 2346.01}]	RowBox[{-, 127.877}]	0.552295	1.83808	0.149017	0	0
0.0699219	0.0368188	25686.	RowBox[{-, 2284.29}]	RowBox[{-, 131.332}]	0.558989	1.86036	0.166126	0	0
0.0699219	0.040166	23129.1	RowBox[{-, 2223.37}]	RowBox[{-, 134.93}]	0.565684	1.88264	0.177595	0	0
0.0699219	0.0435131	21213.6	RowBox[{-, 2163.34}]	RowBox[{-, 138.675}]	0.572378	1.90492	0.186154	0	0
0.0699219	0.0468603	19733.8	RowBox[{-, 2104.27}]	RowBox[{-, 142.568}]	0.579072	1.9272	0.192946	0	0
0.0699219	0.0502075	18570.	RowBox[{-, 2046.23}]	RowBox[{-, 146.611}]	0.585767	1.94948	0.19856	0	0
0.0699219	0.0535546	17645.9	RowBox[{-, 1989.28}]	RowBox[{-, 150.808}]	0.592461	1.97176	0.203339	0	0
0.0699219	0.0569018	16909.1	RowBox[{-, 1933.48}]	RowBox[{-, 155.161}]	0.599155	1.99404	0.2075	0	0

$RowBox[{aluminum, , thrust = , , 500000, , chht , , 0.204822, , vol in^3 = , , 1647.33}]$

rBot	Wall	stress lbf	sp thrust	weight	dia	dia ft	r max stress	min # noz	max # noz
0.0828489	0.00793701	RowBox[{RowBox[{81647.1, }], -, RowBox[{60106.6, , i}]}]	RowBox[{-, 2589.03}]	RowBox[{-, 193.122}]	0.591217	1.96762	RowBox[{RowBox[{0.261859, }], +, RowBox[{0.261859, , i}]}]	0	0
0.0828489	0.0119055	RowBox[{RowBox[{63883.4, }], -, RowBox[{45488.4, , i}]}]	RowBox[{-, 2530.76}]	RowBox[{-, 197.569}]	0.599154	1.99403	RowBox[{RowBox[{0.227802, }], +, RowBox[{0.227802, , i}]}]	0	0
0.0828489	0.015874	RowBox[{RowBox[{55358.5, }], -, RowBox[{35912.7, , i}]}]	RowBox[{-, 2472.44}]	RowBox[{-, 202.23}]	0.607091	2.02045	RowBox[{RowBox[{0.20241, }], +, RowBox[{0.20241, , i}]}]	0	0
0.0828489	0.0198425	RowBox[{RowBox[{50527.3, }], -, RowBox[{28557.6, , i}]}]	RowBox[{-, 2414.21}]	RowBox[{-, 207.107}]	0.615028	2.04686	RowBox[{RowBox[{0.180496, }], +, RowBox[{0.180496, , i}]}]	0	0
0.0828489	0.0277795	RowBox[{RowBox[{45611.9, }], -, RowBox[{16084.8, , i}]}]	RowBox[{-, 2298.55}]	RowBox[{-, 217.528}]	0.630902	2.09969	RowBox[{RowBox[{0.135461, }], +, RowBox[{0.135461, , i}]}]	0	0
0.0828489	0.031748	RowBox[{RowBox[{44340.9, }], -, RowBox[{8821.6, , i}]}]	RowBox[{-, 2241.34}]	RowBox[{-, 223.081}]	0.638839	2.12611	RowBox[{RowBox[{0.100318, }], +, RowBox[{0.100318, , i}]}]	0	0
0.0828489	0.0357165	35313.5	RowBox[{-, 2184.68}]	RowBox[{-, 228.866}]	0.646776	2.15252	0.13675	0	0
0.0828489	0.039685	29305.8	RowBox[{-, 2128.67}]	RowBox[{-, 234.889}]	0.654713	2.17894	0.176679	0	0
0.0828489	0.0436535	25686.	RowBox[{-, 2073.38}]	RowBox[{-, 241.152}]	0.66265	2.20535	0.196965	0	0
0.0828489	0.047622	23129.1	RowBox[{-, 2018.89}]	RowBox[{-, 247.661}]	0.670587	2.23177	0.210562	0	0
0.0828489	0.0515905	21213.6	RowBox[{-, 1965.27}]	RowBox[{-, 254.419}]	0.678524	2.25818	0.22071	0	0
0.0828489	0.055559	19733.8	RowBox[{-, 1912.56}]	RowBox[{-, 261.429}]	0.686461	2.2846	0.228763	0	0
0.0828489	0.0595275	18570.	RowBox[{-, 1860.83}]	RowBox[{-, 268.697}]	0.694398	2.31101	0.235419	0	0
0.0828489	0.063496	17645.9	RowBox[{-, 1810.11}]	RowBox[{-, 276.226}]	0.702335	2.33743	0.241085	0	0
0.0828489	0.0674645	16909.1	RowBox[{-, 1760.44}]	RowBox[{-, 284.02}]	0.710272	2.36384	0.246019	0	0

$RowBox[{aluminum, , thrust = , , 1000000, , chht , , 0.25806, , vol in^3 = , , 3294.66}]$

rBot	Wall	stress lbf	sp thrust	weight	dia	dia ft	r max stress	min # noz	max # noz
0.105409	0.01	RowBox[{RowBox[{81647.1, }], -, RowBox[{60106.6, , i}]}]	RowBox[{-, 2346.5}]	RowBox[{-, 426.166}]	0.746939	2.48587	RowBox[{RowBox[{0.329922, }], +, RowBox[{0.329922, , i}]}]	0	0
0.105409	0.015	RowBox[{RowBox[{63883.4, }], -, RowBox[{45488.4, , i}]}]	RowBox[{-, 2293.15}]	RowBox[{-, 436.082}]	0.756939	2.51916	RowBox[{RowBox[{0.287012, }], +, RowBox[{0.287012, , i}]}]	0	0
0.105409	0.02	RowBox[{RowBox[{55358.5, }], -, RowBox[{35912.7, , i}]}]	RowBox[{-, 2239.96}]	RowBox[{-, 446.436}]	0.766939	2.55244	RowBox[{RowBox[{0.25502, }], +, RowBox[{0.25502, , i}]}]	0	0
0.105409	0.025	RowBox[{RowBox[{50527.3, }], -, RowBox[{28557.6, , i}]}]	RowBox[{-, 2187.05}]	RowBox[{-, 457.237}]	0.776939	2.58572	RowBox[{RowBox[{0.227411, }], +, RowBox[{0.227411, , i}]}]	0	0
0.105409	0.035	RowBox[{RowBox[{45611.9, }], -, RowBox[{16084.8, , i}]}]	RowBox[{-, 2082.41}]	RowBox[{-, 480.212}]	0.796939	2.65228	RowBox[{RowBox[{0.170671, }], +, RowBox[{0.170671, , i}]}]	0	0
0.105409	0.04	RowBox[{RowBox[{44340.9, }], -, RowBox[{8821.6, , i}]}]	RowBox[{-, 2030.86}]	RowBox[{-, 492.401}]	0.806939	2.68556	RowBox[{RowBox[{0.126393, }], +, RowBox[{0.126393, , i}]}]	0	0
0.105409	0.045	35313.5	RowBox[{-, 1979.92}]	RowBox[{-, 505.07}]	0.816939	2.71884	0.172295	0	0
0.105409	0.05	29305.8	RowBox[{-, 1929.66}]	RowBox[{-, 518.225}]	0.826939	2.75212	0.222602	0	0
0.105409	0.055	25686.	RowBox[{-, 1880.14}]	RowBox[{-, 531.876}]	0.836939	2.7854	0.24816	0	0
0.105409	0.06	23129.1	RowBox[{-, 1831.4}]	RowBox[{-, 546.029}]	0.846939	2.81868	0.265291	0	0
0.105409	0.065	21213.6	RowBox[{-, 1783.51}]	RowBox[{-, 560.693}]	0.856939	2.85196	0.278078	0	0
0.105409	0.07	19733.8	RowBox[{-, 1736.48}]	RowBox[{-, 575.876}]	0.866939	2.88524	0.288223	0	0
0.105409	0.075	18570.	RowBox[{-, 1690.37}]	RowBox[{-, 591.587}]	0.876939	2.91853	0.296609	0	0
0.105409	0.08	17645.9	RowBox[{-, 1645.19}]	RowBox[{-, 607.832}]	0.886939	2.95181	0.303747	0	0
0.105409	0.085	16909.1	RowBox[{-, 1600.97}]	RowBox[{-, 624.62}]	0.896939	2.98509	0.309964	0	0

$RowBox[{aluminum, , thrust = , , 1500000, , chht , , 0.295405, , vol in^3 = , , 4942.}]$

rBot	Wall	stress lbf	sp thrust	weight	dia	dia ft	r max stress	min # noz	max # noz
0.121942	0.0114471	RowBox[{RowBox[{81647.1, }], -, RowBox[{60106.6, , i}]}]	RowBox[{-, 2244.09}]	RowBox[{-, 668.421}]	0.857588	2.85412	RowBox[{RowBox[{0.377666, }], +, RowBox[{0.377666, , i}]}]	0	0
0.121942	0.0171707	RowBox[{RowBox[{63883.4, }], -, RowBox[{45488.4, , i}]}]	RowBox[{-, 2192.86}]	RowBox[{-, 684.039}]	0.869035	2.89222	RowBox[{RowBox[{0.328547, }], +, RowBox[{0.328547, , i}]}]	0	0
0.121942	0.0228943	RowBox[{RowBox[{55358.5, }], -, RowBox[{35912.7, , i}]}]	RowBox[{-, 2141.86}]	RowBox[{-, 700.325}]	0.880482	2.93032	RowBox[{RowBox[{0.291925, }], +, RowBox[{0.291925, , i}]}]	0	0
0.121942	0.0286179	RowBox[{RowBox[{50527.3, }], -, RowBox[{28557.6, , i}]}]	RowBox[{-, 2091.2}]	RowBox[{-, 717.29}]	0.891929	2.96842	RowBox[{RowBox[{0.26032, }], +, RowBox[{0.26032, , i}]}]	0	0
0.121942	0.040065	RowBox[{RowBox[{45611.9, }], -, RowBox[{16084.8, , i}]}]	RowBox[{-, 1991.22}]	RowBox[{-, 753.307}]	0.914824	3.04461	RowBox[{RowBox[{0.195369, }], +, RowBox[{0.195369, , i}]}]	0	0
0.121942	0.0457886	RowBox[{RowBox[{44340.9, }], -, RowBox[{8821.6, , i}]}]	RowBox[{-, 1942.04}]	RowBox[{-, 772.383}]	0.926271	3.08271	RowBox[{RowBox[{0.144684, }], +, RowBox[{0.144684, , i}]}]	0	0
0.121942	0.0515121	35313.5	RowBox[{-, 1893.49}]	RowBox[{-, 792.187}]	0.937718	3.1208	0.197228	0	0
0.121942	0.0572357	29305.8	RowBox[{-, 1845.63}]	RowBox[{-, 812.73}]	0.949165	3.1589	0.254816	0	0
0.121942	0.0629593	25686.	RowBox[{-, 1798.51}]	RowBox[{-, 834.025}]	0.960612	3.197	0.284072	0	0
0.121942	0.0686829	23129.1	RowBox[{-, 1752.16}]	RowBox[{-, 856.084}]	0.972059	3.2351	0.303683	0	0
0.121942	0.0744064	21213.6	RowBox[{-, 1706.64}]	RowBox[{-, 878.918}]	0.983506	3.27319	0.318319	0	0
0.121942	0.08013	19733.8	RowBox[{-, 1661.97}]	RowBox[{-, 902.541}]	0.994954	3.31129	0.329933	0	0
0.121942	0.0858536	18570.	RowBox[{-, 1618.19}]	RowBox[{-, 926.963}]	1.0064	3.34939	0.339532	0	0
0.121942	0.0915771	17645.9	RowBox[{-, 1575.31}]	RowBox[{-, 952.197}]	1.01785	3.38748	0.347704	0	0
0.121942	0.0973007	16909.1	RowBox[{-, 1533.34}]	RowBox[{-, 978.254}]	1.0293	3.42558	0.354821	0	0

$RowBox[{aluminum, , thrust = , , 2000000, , chht , , 0.325135, , vol in^3 = , , 6589.33}]$

rBot	Wall	stress lbf	sp thrust	weight	dia	dia ft	r max stress	min # noz	max # noz
0.135477	0.0125992	RowBox[{RowBox[{81647.1, }], -, RowBox[{60106.6, , i}]}]	RowBox[{-, 2183.82}]	RowBox[{-, 915.826}]	0.946423	3.14978	RowBox[{RowBox[{0.415676, }], +, RowBox[{0.415676, , i}]}]	0	0
0.135477	0.0188988	RowBox[{RowBox[{63883.4, }], -, RowBox[{45488.4, , i}]}]	RowBox[{-, 2133.84}]	RowBox[{-, 937.278}]	0.959022	3.19171	RowBox[{RowBox[{0.361613, }], +, RowBox[{0.361613, , i}]}]	0	0
0.135477	0.0251984	RowBox[{RowBox[{55358.5, }], -, RowBox[{35912.7, , i}]}]	RowBox[{-, 2084.14}]	RowBox[{-, 959.627}]	0.971621	3.23364	RowBox[{RowBox[{0.321305, }], +, RowBox[{0.321305, , i}]}]	0	0
0.135477	0.031498	RowBox[{RowBox[{50527.3, }], -, RowBox[{28557.6, , i}]}]	RowBox[{-, 2034.81}]	RowBox[{-, 982.891}]	0.984221	3.27557	RowBox[{RowBox[{0.28652, }], +, RowBox[{0.28652, , i}]}]	0	0
0.135477	0.0440972	RowBox[{RowBox[{45611.9, }], -, RowBox[{16084.8, , i}]}]	RowBox[{-, 1937.56}]	RowBox[{-, 1032.22}]	1.00942	3.35943	RowBox[{RowBox[{0.215031, }], +, RowBox[{0.215031, , i}]}]	0	0
0.135477	0.0503968	RowBox[{RowBox[{44340.9, }], -, RowBox[{8821.6, , i}]}]	RowBox[{-, 1889.78}]	RowBox[{-, 1058.33}]	1.02202	3.40136	RowBox[{RowBox[{0.159246, }], +, RowBox[{0.159246, , i}]}]	0	0
0.135477	0.0566964	35313.5	RowBox[{-, 1842.63}]	RowBox[{-, 1085.4}]	1.03462	3.44329	0.217078	0	0
0.135477	0.0629961	29305.8	RowBox[{-, 1796.17}]	RowBox[{-, 1113.48}]	1.04722	3.48522	0.280461	0	0
0.135477	0.0692957	25686.	RowBox[{-, 1750.45}]	RowBox[{-, 1142.56}]	1.05982	3.52716	0.312662	0	0
0.135477	0.0755953	23129.1	RowBox[{-, 1705.51}]	RowBox[{-, 1172.67}]	1.07242	3.56909	0.334246	0	0
0.135477	0.0818949	21213.6	RowBox[{-, 1661.37}]	RowBox[{-, 1203.82}]	1.08501	3.61102	0.350356	0	0
0.135477	0.0881945	19733.8	RowBox[{-, 1618.08}]	RowBox[{-, 1236.03}]	1.09761	3.65295	0.363139	0	0
0.135477	0.0944941	18570.	RowBox[{-, 1575.65}]	RowBox[{-, 1269.32}]	1.11021	3.69488	0.373704	0	0
0.135477	0.100794	17645.9	RowBox[{-, 1534.1}]	RowBox[{-, 1303.69}]	1.12281	3.73681	0.382698	0	0
0.135477	0.107093	16909.1	RowBox[{-, 1493.46}]	RowBox[{-, 1339.17}]	1.13541	3.77874	0.390531	0	0

$RowBox[{aluminum, , thrust = , , 3000000, , chht , , 0.372187, , vol in^3 = , , 9883.99}]$

rBot	Wall	stress lbf	sp thrust	weight	dia	dia ft	r max stress	min # noz	max # noz
0.157522	0.0144225	RowBox[{RowBox[{81647.1, }], -, RowBox[{60106.6, , i}]}]	RowBox[{-, 2112.5}]	RowBox[{-, 1420.12}]	1.08826	3.62183	RowBox[{RowBox[{0.47583, }], +, RowBox[{0.47583, , i}]}]	0	0
0.157522	0.0216337	RowBox[{RowBox[{63883.4, }], -, RowBox[{45488.4, , i}]}]	RowBox[{-, 2064.01}]	RowBox[{-, 1453.48}]	1.10269	3.66983	RowBox[{RowBox[{0.413943, }], +, RowBox[{0.413943, , i}]}]	0	0
0.157522	0.028845	RowBox[{RowBox[{55358.5, }], -, RowBox[{35912.7, , i}]}]	RowBox[{-, 2015.86}]	RowBox[{-, 1488.2}]	1.11711	3.71783	RowBox[{RowBox[{0.367803, }], +, RowBox[{0.367803, , i}]}]	0	0
0.157522	0.0360562	RowBox[{RowBox[{50527.3, }], -, RowBox[{28557.6, , i}]}]	RowBox[{-, 1968.11}]	RowBox[{-, 1524.31}]	1.13153	3.76583	RowBox[{RowBox[{0.327983, }], +, RowBox[{0.327983, , i}]}]	0	0
0.157522	0.0504787	RowBox[{RowBox[{45611.9, }], -, RowBox[{16084.8, , i}]}]	RowBox[{-, 1874.09}]	RowBox[{-, 1600.78}]	1.16038	3.86183	RowBox[{RowBox[{0.246149, }], +, RowBox[{0.246149, , i}]}]	0	0
0.157522	0.05769	RowBox[{RowBox[{44340.9, }], -, RowBox[{8821.6, , i}]}]	RowBox[{-, 1827.95}]	RowBox[{-, 1641.19}]	1.1748	3.90983	RowBox[{RowBox[{0.182291, }], +, RowBox[{0.182291, , i}]}]	0	0
0.157522	0.0649012	35313.5	RowBox[{-, 1782.45}]	RowBox[{-, 1683.08}]	1.18922	3.95782	0.248492	0	0
0.157522	0.0721125	29305.8	RowBox[{-, 1737.65}]	RowBox[{-, 1726.47}]	1.20364	4.00582	0.321047	0	0
0.157522	0.0793237	25686.	RowBox[{-, 1693.58}]	RowBox[{-, 1771.4}]	1.21807	4.05382	0.357909	0	0
0.157522	0.086535	23129.1	RowBox[{-, 1650.27}]	RowBox[{-, 1817.88}]	1.23249	4.10182	0.382616	0	0
0.157522	0.0937462	21213.6	RowBox[{-, 1607.77}]	RowBox[{-, 1865.94}]	1.24691	4.14982	0.401057	0	0
0.157522	0.100957	19733.8	RowBox[{-, 1566.09}]	RowBox[{-, 1915.6}]	1.26133	4.19782	0.41569	0	0
0.157522	0.108169	18570.	RowBox[{-, 1525.25}]	RowBox[{-, 1966.89}]	1.27576	4.24582	0.427784	0	0
0.157522	0.11538	17645.9	RowBox[{-, 1485.28}]	RowBox[{-, 2019.82}]	1.29018	4.29382	0.43808	0	0
0.157522	0.122591	16909.1	RowBox[{-, 1446.18}]	RowBox[{-, 2074.43}]	1.3046	4.34182	0.447046	0	0

$RowBox[{aluminum, , thrust = , , 5000000, , chht , , 0.441276, , vol in^3 = , , 16473.3}]$

rBot	Wall	stress lbf	sp thrust	weight	dia	dia ft	r max stress	min # noz	max # noz
0.191163	0.0170998	RowBox[{RowBox[{81647.1, }], -, RowBox[{60106.6, , i}]}]	RowBox[{-, 2040.34}]	RowBox[{-, 2450.57}]	1.29908	4.32344	RowBox[{RowBox[{0.564159, }], +, RowBox[{0.564159, , i}]}]	0	0
0.191163	0.0256496	RowBox[{RowBox[{63883.4, }], -, RowBox[{45488.4, , i}]}]	RowBox[{-, 1993.38}]	RowBox[{-, 2508.3}]	1.31618	4.38035	RowBox[{RowBox[{0.490784, }], +, RowBox[{0.490784, , i}]}]	0	0
0.191163	0.0341995	RowBox[{RowBox[{55358.5, }], -, RowBox[{35912.7, , i}]}]	RowBox[{-, 1946.79}]	RowBox[{-, 2568.33}]	1.33328	4.43726	RowBox[{RowBox[{0.436078, }], +, RowBox[{0.436078, , i}]}]	0	0
0.191163	0.0427494	RowBox[{RowBox[{50527.3, }], -, RowBox[{28557.6, , i}]}]	RowBox[{-, 1900.64}]	RowBox[{-, 2630.69}]	1.35038	4.49417	RowBox[{RowBox[{0.388867, }], +, RowBox[{0.388867, , i}]}]	0	0
0.191163	0.0598492	RowBox[{RowBox[{45611.9, }], -, RowBox[{16084.8, , i}]}]	RowBox[{-, 1809.89}]	RowBox[{-, 2762.59}]	1.38458	4.60799	RowBox[{RowBox[{0.291842, }], +, RowBox[{0.291842, , i}]}]	0	0
0.191163	0.068399	RowBox[{RowBox[{44340.9, }], -, RowBox[{8821.6, , i}]}]	RowBox[{-, 1765.41}]	RowBox[{-, 2832.21}]	1.40168	4.6649	RowBox[{RowBox[{0.216129, }], +, RowBox[{0.216129, , i}]}]	0	0
0.191163	0.0769489	35313.5	RowBox[{-, 1721.58}]	RowBox[{-, 2904.32}]	1.41878	4.72181	0.29462	0	0
0.191163	0.0854988	29305.8	RowBox[{-, 1678.44}]	RowBox[{-, 2978.96}]	1.43588	4.77872	0.380644	0	0
0.191163	0.0940487	25686.	RowBox[{-, 1636.03}]	RowBox[{-, 3056.19}]	1.45298	4.83563	0.424348	0	0
0.191163	0.102599	23129.1	RowBox[{-, 1594.37}]	RowBox[{-, 3136.03}]	1.47008	4.89254	0.453642	0	0
0.191163	0.111148	21213.6	RowBox[{-, 1553.51}]	RowBox[{-, 3218.52}]	1.48718	4.94945	0.475506	0	0
0.191163	0.119698	19733.8	RowBox[{-, 1513.45}]	RowBox[{-, 3303.72}]	1.50428	5.00636	0.492855	0	0
0.191163	0.128248	18570.	RowBox[{-, 1474.21}]	RowBox[{-, 3391.65}]	1.52138	5.06327	0.507194	0	0
0.191163	0.136798	17645.9	RowBox[{-, 1435.81}]	RowBox[{-, 3482.35}]	1.53848	5.12018	0.519401	0	0
0.191163	0.145348	16909.1	RowBox[{-, 1398.26}]	RowBox[{-, 3575.88}]	1.55558	5.17708	0.530032	0	0

ω =. ; radialelongation = . ; modulusElasticity =. ; μ = . ; ρ = . ; r &nb ... ]]}], ;, , almaxtstress = {}, ;}], , , )}]}], ]}]}], , )}]}], ]}]

$RowBox[{aluminum, , thrust = , , 10, , vol in^3 = , , 0.0329466}]$

rBot	Wall	stress lbf	sp thrust	weight	dia	r max stress	min # noz	max # noz
0.0005	0.00107722	29305.8	150.228	0.0665655	0.0142739	0.00479581	0	0
0.0005	0.00129266	23129.1	142.379	0.0702351	0.0147048	0.00571553	0	0
0.0005	0.00140038	21213.6	138.704	0.0720958	0.0149202	0.005991	0	0
0.0005	0.0015081	19733.8	135.183	0.0739736	0.0151357	0.00620958	0	0
0.0005	0.00161583	18570.	131.807	0.0758685	0.0153511	0.00639024	0	0
0.0005	0.00172355	17645.9	128.567	0.0777804	0.0155666	0.00654404	0	0
0.0005	0.00183127	16909.1	125.456	0.0797091	0.015782	0.00667798	0	0
0.0005	0.00193899	16322.4	122.467	0.0816547	0.0159975	0.00679675	0	0
0.0005	0.00215443	15496.4	116.828	0.0855959	0.0164283	0.00700101	0	0
0.0006	0.00107722	29305.8	150.228	0.0665655	0.0144739	0.00479581	0	0
0.0006	0.00129266	23129.1	142.379	0.0702351	0.0149048	0.00571553	0	0
0.0006	0.00140038	21213.6	138.704	0.0720958	0.0151202	0.005991	0	0
0.0006	0.0015081	19733.8	135.183	0.0739736	0.0153357	0.00620958	0	0
0.0006	0.00161583	18570.	131.807	0.0758685	0.0155511	0.00639024	0	0
0.0006	0.00172355	17645.9	128.567	0.0777804	0.0157666	0.00654404	0	0
0.0006	0.00183127	16909.1	125.456	0.0797091	0.015982	0.00667798	0	0
0.0006	0.00193899	16322.4	122.467	0.0816547	0.0161975	0.00679675	0	0
0.0006	0.00215443	15496.4	116.828	0.0855959	0.0166283	0.00700101	0	0
0.00065	0.00107722	29305.8	150.228	0.0665655	0.0145739	0.00479581	0	0
0.00065	0.00129266	23129.1	142.379	0.0702351	0.0150048	0.00571553	0	0
0.00065	0.00140038	21213.6	138.704	0.0720958	0.0152202	0.005991	0	0
0.00065	0.0015081	19733.8	135.183	0.0739736	0.0154357	0.00620958	0	0
0.00065	0.00161583	18570.	131.807	0.0758685	0.0156511	0.00639024	0	0
0.00065	0.00172355	17645.9	128.567	0.0777804	0.0158666	0.00654404	0	0
0.00065	0.00183127	16909.1	125.456	0.0797091	0.016082	0.00667798	0	0
0.00065	0.00193899	16322.4	122.467	0.0816547	0.0162975	0.00679675	0	0
0.00065	0.00215443	15496.4	116.828	0.0855959	0.0167283	0.00700101	0	0
0.0007	0.00107722	29305.8	150.228	0.0665655	0.0146739	0.00479581	0	0
0.0007	0.00129266	23129.1	142.379	0.0702351	0.0151048	0.00571553	0	0
0.0007	0.00140038	21213.6	138.704	0.0720958	0.0153202	0.005991	0	0
0.0007	0.0015081	19733.8	135.183	0.0739736	0.0155357	0.00620958	0	0
0.0007	0.00161583	18570.	131.807	0.0758685	0.0157511	0.00639024	0	0
0.0007	0.00172355	17645.9	128.567	0.0777804	0.0159666	0.00654404	0	0
0.0007	0.00183127	16909.1	125.456	0.0797091	0.016182	0.00667798	0	0
0.0007	0.00193899	16322.4	122.467	0.0816547	0.0163975	0.00679675	0	0
0.0007	0.00215443	15496.4	116.828	0.0855959	0.0168283	0.00700101	0	0
0.00075	0.00107722	29305.8	150.228	0.0665655	0.0147739	0.00479581	0	0
0.00075	0.00129266	23129.1	142.379	0.0702351	0.0152048	0.00571553	0	0
0.00075	0.00140038	21213.6	138.704	0.0720958	0.0154202	0.005991	0	0
0.00075	0.0015081	19733.8	135.183	0.0739736	0.0156357	0.00620958	0	0
0.00075	0.00161583	18570.	131.807	0.0758685	0.0158511	0.00639024	0	0
0.00075	0.00172355	17645.9	128.567	0.0777804	0.0160666	0.00654404	0	0
0.00075	0.00183127	16909.1	125.456	0.0797091	0.016282	0.00667798	0	0
0.00075	0.00193899	16322.4	122.467	0.0816547	0.0164975	0.00679675	0	0
0.00075	0.00215443	15496.4	116.828	0.0855959	0.0169283	0.00700101	0	0
0.0008	0.00107722	29305.8	150.228	0.0665655	0.0148739	0.00479581	0	0
0.0008	0.00129266	23129.1	142.379	0.0702351	0.0153048	0.00571553	0	0
0.0008	0.00140038	21213.6	138.704	0.0720958	0.0155202	0.005991	0	0
0.0008	0.0015081	19733.8	135.183	0.0739736	0.0157357	0.00620958	0	0
0.0008	0.00161583	18570.	131.807	0.0758685	0.0159511	0.00639024	0	0
0.0008	0.00172355	17645.9	128.567	0.0777804	0.0161666	0.00654404	0	0
0.0008	0.00183127	16909.1	125.456	0.0797091	0.016382	0.00667798	0	0
0.0008	0.00193899	16322.4	122.467	0.0816547	0.0165975	0.00679675	0	0
0.0008	0.00215443	15496.4	116.828	0.0855959	0.0170283	0.00700101	0	0
0.00085	0.00107722	29305.8	150.228	0.0665655	0.0149739	0.00479581	0	0
0.00085	0.00129266	23129.1	142.379	0.0702351	0.0154048	0.00571553	0	0
0.00085	0.00140038	21213.6	138.704	0.0720958	0.0156202	0.005991	0	0
0.00085	0.0015081	19733.8	135.183	0.0739736	0.0158357	0.00620958	0	0
0.00085	0.00161583	18570.	131.807	0.0758685	0.0160511	0.00639024	0	0
0.00085	0.00172355	17645.9	128.567	0.0777804	0.0162666	0.00654404	0	0
0.00085	0.00183127	16909.1	125.456	0.0797091	0.016482	0.00667798	0	0
0.00085	0.00193899	16322.4	122.467	0.0816547	0.0166975	0.00679675	0	0
0.00085	0.00215443	15496.4	116.828	0.0855959	0.0171283	0.00700101	0	0
0.0009	0.00107722	29305.8	150.228	0.0665655	0.0150739	0.00479581	0	0
0.0009	0.00129266	23129.1	142.379	0.0702351	0.0155048	0.00571553	0	0
0.0009	0.00140038	21213.6	138.704	0.0720958	0.0157202	0.005991	0	0
0.0009	0.0015081	19733.8	135.183	0.0739736	0.0159357	0.00620958	0	0
0.0009	0.00161583	18570.	131.807	0.0758685	0.0161511	0.00639024	0	0
0.0009	0.00172355	17645.9	128.567	0.0777804	0.0163666	0.00654404	0	0
0.0009	0.00183127	16909.1	125.456	0.0797091	0.016582	0.00667798	0	0
0.0009	0.00193899	16322.4	122.467	0.0816547	0.0167975	0.00679675	0	0
0.0009	0.00215443	15496.4	116.828	0.0855959	0.0172283	0.00700101	0	0
0.001	0.00107722	29305.8	150.228	0.0665655	0.0152739	0.00479581	0	0
0.001	0.00129266	23129.1	142.379	0.0702351	0.0157048	0.00571553	0	0
0.001	0.00140038	21213.6	138.704	0.0720958	0.0159202	0.005991	0	0
0.001	0.0015081	19733.8	135.183	0.0739736	0.0161357	0.00620958	0	0
0.001	0.00161583	18570.	131.807	0.0758685	0.0163511	0.00639024	0	0
0.001	0.00172355	17645.9	128.567	0.0777804	0.0165666	0.00654404	0	0
0.001	0.00183127	16909.1	125.456	0.0797091	0.016782	0.00667798	0	0
0.001	0.00193899	16322.4	122.467	0.0816547	0.0169975	0.00679675	0	0
0.001	0.00215443	15496.4	116.828	0.0855959	0.0174283	0.00700101	0	0

$RowBox[{aluminum, , thrust = , , 100, , vol in^3 = , , 0.329466}]$

rBot	Wall	stress lbf	sp thrust	weight	dia	r max stress	min # noz	max # noz
0.00158114	0.00232079	29305.8	327.987	0.30489	0.03176	0.0103323	0	0
0.00158114	0.00278495	23129.1	312.532	0.319968	0.0326884	0.0123137	0	0
0.00158114	0.00301703	21213.6	305.267	0.327582	0.0331525	0.0129072	0	0
0.00158114	0.00324911	19733.8	298.29	0.335245	0.0336167	0.0133781	0	0
0.00158114	0.00348119	18570.	291.583	0.342956	0.0340808	0.0137674	0	0
0.00158114	0.00371327	17645.9	285.132	0.350715	0.034545	0.0140987	0	0
0.00158114	0.00394535	16909.1	278.924	0.35852	0.0350092	0.0143873	0	0
0.00158114	0.00417743	16322.4	272.947	0.366372	0.0354733	0.0146432	0	0
0.00158114	0.00464159	15496.4	261.637	0.382209	0.0364016	0.0150832	0	0
0.00189737	0.00232079	29305.8	327.987	0.30489	0.0323925	0.0103323	0	0
0.00189737	0.00278495	23129.1	312.532	0.319968	0.0333208	0.0123137	0	0
0.00189737	0.00301703	21213.6	305.267	0.327582	0.033785	0.0129072	0	0
0.00189737	0.00324911	19733.8	298.29	0.335245	0.0342491	0.0133781	0	0
0.00189737	0.00348119	18570.	291.583	0.342956	0.0347133	0.0137674	0	0
0.00189737	0.00371327	17645.9	285.132	0.350715	0.0351774	0.0140987	0	0
0.00189737	0.00394535	16909.1	278.924	0.35852	0.0356416	0.0143873	0	0
0.00189737	0.00417743	16322.4	272.947	0.366372	0.0361058	0.0146432	0	0
0.00189737	0.00464159	15496.4	261.637	0.382209	0.0370341	0.0150832	0	0
0.00205548	0.00232079	29305.8	327.987	0.30489	0.0327087	0.0103323	0	0
0.00205548	0.00278495	23129.1	312.532	0.319968	0.033637	0.0123137	0	0
0.00205548	0.00301703	21213.6	305.267	0.327582	0.0341012	0.0129072	0	0
0.00205548	0.00324911	19733.8	298.29	0.335245	0.0345654	0.0133781	0	0
0.00205548	0.00348119	18570.	291.583	0.342956	0.0350295	0.0137674	0	0
0.00205548	0.00371327	17645.9	285.132	0.350715	0.0354937	0.0140987	0	0
0.00205548	0.00394535	16909.1	278.924	0.35852	0.0359578	0.0143873	0	0
0.00205548	0.00417743	16322.4	272.947	0.366372	0.036422	0.0146432	0	0
0.00205548	0.00464159	15496.4	261.637	0.382209	0.0373503	0.0150832	0	0
0.00221359	0.00232079	29305.8	327.987	0.30489	0.0330249	0.0103323	0	0
0.00221359	0.00278495	23129.1	312.532	0.319968	0.0339533	0.0123137	0	0
0.00221359	0.00301703	21213.6	305.267	0.327582	0.0344174	0.0129072	0	0
0.00221359	0.00324911	19733.8	298.29	0.335245	0.0348816	0.0133781	0	0
0.00221359	0.00348119	18570.	291.583	0.342956	0.0353457	0.0137674	0	0
0.00221359	0.00371327	17645.9	285.132	0.350715	0.0358099	0.0140987	0	0
0.00221359	0.00394535	16909.1	278.924	0.35852	0.0362741	0.0143873	0	0
0.00221359	0.00417743	16322.4	272.947	0.366372	0.0367382	0.0146432	0	0
0.00221359	0.00464159	15496.4	261.637	0.382209	0.0376665	0.0150832	0	0
0.00237171	0.00232079	29305.8	327.987	0.30489	0.0333412	0.0103323	0	0
0.00237171	0.00278495	23129.1	312.532	0.319968	0.0342695	0.0123137	0	0
0.00237171	0.00301703	21213.6	305.267	0.327582	0.0347337	0.0129072	0	0
0.00237171	0.00324911	19733.8	298.29	0.335245	0.0351978	0.0133781	0	0
0.00237171	0.00348119	18570.	291.583	0.342956	0.035662	0.0137674	0	0
0.00237171	0.00371327	17645.9	285.132	0.350715	0.0361261	0.0140987	0	0
0.00237171	0.00394535	16909.1	278.924	0.35852	0.0365903	0.0143873	0	0
0.00237171	0.00417743	16322.4	272.947	0.366372	0.0370544	0.0146432	0	0
0.00237171	0.00464159	15496.4	261.637	0.382209	0.0379828	0.0150832	0	0
0.00252982	0.00232079	29305.8	327.987	0.30489	0.0336574	0.0103323	0	0
0.00252982	0.00278495	23129.1	312.532	0.319968	0.0345857	0.0123137	0	0
0.00252982	0.00301703	21213.6	305.267	0.327582	0.0350499	0.0129072	0	0
0.00252982	0.00324911	19733.8	298.29	0.335245	0.035514	0.0133781	0	0
0.00252982	0.00348119	18570.	291.583	0.342956	0.0359782	0.0137674	0	0
0.00252982	0.00371327	17645.9	285.132	0.350715	0.0364424	0.0140987	0	0
0.00252982	0.00394535	16909.1	278.924	0.35852	0.0369065	0.0143873	0	0
0.00252982	0.00417743	16322.4	272.947	0.366372	0.0373707	0.0146432	0	0
0.00252982	0.00464159	15496.4	261.637	0.382209	0.038299	0.0150832	0	0
0.00268794	0.00232079	29305.8	327.987	0.30489	0.0339736	0.0103323	0	0
0.00268794	0.00278495	23129.1	312.532	0.319968	0.034902	0.0123137	0	0
0.00268794	0.00301703	21213.6	305.267	0.327582	0.0353661	0.0129072	0	0
0.00268794	0.00324911	19733.8	298.29	0.335245	0.0358303	0.0133781	0	0
0.00268794	0.00348119	18570.	291.583	0.342956	0.0362944	0.0137674	0	0
0.00268794	0.00371327	17645.9	285.132	0.350715	0.0367586	0.0140987	0	0
0.00268794	0.00394535	16909.1	278.924	0.35852	0.0372227	0.0143873	0	0
0.00268794	0.00417743	16322.4	272.947	0.366372	0.0376869	0.0146432	0	0
0.00268794	0.00464159	15496.4	261.637	0.382209	0.0386152	0.0150832	0	0
0.00284605	0.00232079	29305.8	327.987	0.30489	0.0342899	0.0103323	0	0
0.00284605	0.00278495	23129.1	312.532	0.319968	0.0352182	0.0123137	0	0
0.00284605	0.00301703	21213.6	305.267	0.327582	0.0356823	0.0129072	0	0
0.00284605	0.00324911	19733.8	298.29	0.335245	0.0361465	0.0133781	0	0
0.00284605	0.00348119	18570.	291.583	0.342956	0.0366107	0.0137674	0	0
0.00284605	0.00371327	17645.9	285.132	0.350715	0.0370748	0.0140987	0	0
0.00284605	0.00394535	16909.1	278.924	0.35852	0.037539	0.0143873	0	0
0.00284605	0.00417743	16322.4	272.947	0.366372	0.0380031	0.0146432	0	0
0.00284605	0.00464159	15496.4	261.637	0.382209	0.0389314	0.0150832	0	0
0.00316228	0.00232079	29305.8	327.987	0.30489	0.0349223	0.0103323	0	0
0.00316228	0.00278495	23129.1	312.532	0.319968	0.0358506	0.0123137	0	0
0.00316228	0.00301703	21213.6	305.267	0.327582	0.0363148	0.0129072	0	0
0.00316228	0.00324911	19733.8	298.29	0.335245	0.036779	0.0133781	0	0
0.00316228	0.00348119	18570.	291.583	0.342956	0.0372431	0.0137674	0	0
0.00316228	0.00371327	17645.9	285.132	0.350715	0.0377073	0.0140987	0	0
0.00316228	0.00394535	16909.1	278.924	0.35852	0.0381714	0.0143873	0	0
0.00316228	0.00417743	16322.4	272.947	0.366372	0.0386356	0.0146432	0	0
0.00316228	0.00464159	15496.4	261.637	0.382209	0.0395639	0.0150832	0	0

$RowBox[{aluminum, , thrust = , , 400, , vol in^3 = , , 1.31787}]$

rBot	Wall	stress lbf	sp thrust	weight	dia	r max stress	min # noz	max # noz
0.00316228	0.00368403	29305.8	578.789	0.691099	0.0517207	0.0164014	0	0
0.00316228	0.00442084	23129.1	552.723	0.723689	0.0531943	0.0195468	0	0
0.00316228	0.00478924	21213.6	540.504	0.740051	0.0539311	0.0204889	0	0
0.00316228	0.00515764	19733.8	528.785	0.756451	0.0546679	0.0212365	0	0
0.00316228	0.00552605	18570.	517.539	0.772889	0.0554047	0.0218543	0	0
0.00316228	0.00589445	17645.9	506.74	0.789359	0.0561415	0.0223803	0	0
0.00316228	0.00626285	16909.1	496.365	0.805859	0.0568783	0.0228384	0	0
0.00316228	0.00663126	16322.4	486.389	0.822387	0.0576151	0.0232446	0	0
0.00316228	0.00736806	15496.4	467.558	0.855508	0.0590887	0.0239431	0	0
0.00379473	0.00368403	29305.8	578.789	0.691099	0.0529856	0.0164014	0	0
0.00379473	0.00442084	23129.1	552.723	0.723689	0.0544592	0.0195468	0	0
0.00379473	0.00478924	21213.6	540.504	0.740051	0.055196	0.0204889	0	0
0.00379473	0.00515764	19733.8	528.785	0.756451	0.0559328	0.0212365	0	0
0.00379473	0.00552605	18570.	517.539	0.772889	0.0566696	0.0218543	0	0
0.00379473	0.00589445	17645.9	506.74	0.789359	0.0574064	0.0223803	0	0
0.00379473	0.00626285	16909.1	496.365	0.805859	0.0581432	0.0228384	0	0
0.00379473	0.00663126	16322.4	486.389	0.822387	0.05888	0.0232446	0	0
0.00379473	0.00736806	15496.4	467.558	0.855508	0.0603536	0.0239431	0	0
0.00411096	0.00368403	29305.8	578.789	0.691099	0.053618	0.0164014	0	0
0.00411096	0.00442084	23129.1	552.723	0.723689	0.0550916	0.0195468	0	0
0.00411096	0.00478924	21213.6	540.504	0.740051	0.0558285	0.0204889	0	0
0.00411096	0.00515764	19733.8	528.785	0.756451	0.0565653	0.0212365	0	0
0.00411096	0.00552605	18570.	517.539	0.772889	0.0573021	0.0218543	0	0
0.00411096	0.00589445	17645.9	506.74	0.789359	0.0580389	0.0223803	0	0
0.00411096	0.00626285	16909.1	496.365	0.805859	0.0587757	0.0228384	0	0
0.00411096	0.00663126	16322.4	486.389	0.822387	0.0595125	0.0232446	0	0
0.00411096	0.00736806	15496.4	467.558	0.855508	0.0609861	0.0239431	0	0
0.00442719	0.00368403	29305.8	578.789	0.691099	0.0542505	0.0164014	0	0
0.00442719	0.00442084	23129.1	552.723	0.723689	0.0557241	0.0195468	0	0
0.00442719	0.00478924	21213.6	540.504	0.740051	0.0564609	0.0204889	0	0
0.00442719	0.00515764	19733.8	528.785	0.756451	0.0571977	0.0212365	0	0
0.00442719	0.00552605	18570.	517.539	0.772889	0.0579345	0.0218543	0	0
0.00442719	0.00589445	17645.9	506.74	0.789359	0.0586713	0.0223803	0	0
0.00442719	0.00626285	16909.1	496.365	0.805859	0.0594081	0.0228384	0	0
0.00442719	0.00663126	16322.4	486.389	0.822387	0.0601449	0.0232446	0	0
0.00442719	0.00736806	15496.4	467.558	0.855508	0.0616186	0.0239431	0	0
0.00474342	0.00368403	29305.8	578.789	0.691099	0.0548829	0.0164014	0	0
0.00474342	0.00442084	23129.1	552.723	0.723689	0.0563566	0.0195468	0	0
0.00474342	0.00478924	21213.6	540.504	0.740051	0.0570934	0.0204889	0	0
0.00474342	0.00515764	19733.8	528.785	0.756451	0.0578302	0.0212365	0	0
0.00474342	0.00552605	18570.	517.539	0.772889	0.058567	0.0218543	0	0
0.00474342	0.00589445	17645.9	506.74	0.789359	0.0593038	0.0223803	0	0
0.00474342	0.00626285	16909.1	496.365	0.805859	0.0600406	0.0228384	0	0
0.00474342	0.00663126	16322.4	486.389	0.822387	0.0607774	0.0232446	0	0
0.00474342	0.00736806	15496.4	467.558	0.855508	0.062251	0.0239431	0	0
0.00505964	0.00368403	29305.8	578.789	0.691099	0.0555154	0.0164014	0	0
0.00505964	0.00442084	23129.1	552.723	0.723689	0.056989	0.0195468	0	0
0.00505964	0.00478924	21213.6	540.504	0.740051	0.0577258	0.0204889	0	0
0.00505964	0.00515764	19733.8	528.785	0.756451	0.0584626	0.0212365	0	0
0.00505964	0.00552605	18570.	517.539	0.772889	0.0591994	0.0218543	0	0
0.00505964	0.00589445	17645.9	506.74	0.789359	0.0599362	0.0223803	0	0
0.00505964	0.00626285	16909.1	496.365	0.805859	0.060673	0.0228384	0	0
0.00505964	0.00663126	16322.4	486.389	0.822387	0.0614099	0.0232446	0	0
0.00505964	0.00736806	15496.4	467.558	0.855508	0.0628835	0.0239431	0	0
0.00537587	0.00368403	29305.8	578.789	0.691099	0.0561479	0.0164014	0	0
0.00537587	0.00442084	23129.1	552.723	0.723689	0.0576215	0.0195468	0	0
0.00537587	0.00478924	21213.6	540.504	0.740051	0.0583583	0.0204889	0	0
0.00537587	0.00515764	19733.8	528.785	0.756451	0.0590951	0.0212365	0	0
0.00537587	0.00552605	18570.	517.539	0.772889	0.0598319	0.0218543	0	0
0.00537587	0.00589445	17645.9	506.74	0.789359	0.0605687	0.0223803	0	0
0.00537587	0.00626285	16909.1	496.365	0.805859	0.0613055	0.0228384	0	0
0.00537587	0.00663126	16322.4	486.389	0.822387	0.0620423	0.0232446	0	0
0.00537587	0.00736806	15496.4	467.558	0.855508	0.0635159	0.0239431	0	0
0.0056921	0.00368403	29305.8	578.789	0.691099	0.0567803	0.0164014	0	0
0.0056921	0.00442084	23129.1	552.723	0.723689	0.0582539	0.0195468	0	0
0.0056921	0.00478924	21213.6	540.504	0.740051	0.0589907	0.0204889	0	0
0.0056921	0.00515764	19733.8	528.785	0.756451	0.0597275	0.0212365	0	0
0.0056921	0.00552605	18570.	517.539	0.772889	0.0604643	0.0218543	0	0
0.0056921	0.00589445	17645.9	506.74	0.789359	0.0612012	0.0223803	0	0
0.0056921	0.00626285	16909.1	496.365	0.805859	0.061938	0.0228384	0	0
0.0056921	0.00663126	16322.4	486.389	0.822387	0.0626748	0.0232446	0	0
0.0056921	0.00736806	15496.4	467.558	0.855508	0.0641484	0.0239431	0	0
0.00632456	0.00368403	29305.8	578.789	0.691099	0.0580452	0.0164014	0	0
0.00632456	0.00442084	23129.1	552.723	0.723689	0.0595188	0.0195468	0	0
0.00632456	0.00478924	21213.6	540.504	0.740051	0.0602556	0.0204889	0	0
0.00632456	0.00515764	19733.8	528.785	0.756451	0.0609925	0.0212365	0	0
0.00632456	0.00552605	18570.	517.539	0.772889	0.0617293	0.0218543	0	0
0.00632456	0.00589445	17645.9	506.74	0.789359	0.0624661	0.0223803	0	0
0.00632456	0.00626285	16909.1	496.365	0.805859	0.0632029	0.0228384	0	0
0.00632456	0.00663126	16322.4	486.389	0.822387	0.0639397	0.0232446	0	0
0.00632456	0.00736806	15496.4	467.558	0.855508	0.0654133	0.0239431	0	0

$RowBox[{aluminum, , thrust = , , 500, , vol in^3 = , , 1.64733}]$

rBot	Wall	stress lbf	sp thrust	weight	dia	r max stress	min # noz	max # noz
0.00353553	0.0039685	29305.8	640.596	0.780523	0.0559725	0.0176679	0	0
0.00353553	0.0047622	23129.1	611.97	0.817033	0.05756	0.0210562	0	0
0.00353553	0.00515905	21213.6	598.563	0.835335	0.0583537	0.022071	0	0
0.00353553	0.0055559	19733.8	585.712	0.853662	0.0591474	0.0228763	0	0
0.00353553	0.00595275	18570.	573.388	0.87201	0.0599411	0.0235419	0	0
0.00353553	0.0063496	17645.9	561.56	0.890377	0.0607348	0.0241085	0	0
0.00353553	0.00674645	16909.1	550.202	0.908756	0.0615285	0.0246019	0	0
0.00353553	0.0071433	16322.4	539.29	0.927146	0.0623222	0.0250395	0	0
0.00353553	0.00793701	15496.4	518.706	0.963937	0.0639096	0.025792	0	0
0.00424264	0.0039685	29305.8	640.596	0.780523	0.0573868	0.0176679	0	0
0.00424264	0.0047622	23129.1	611.97	0.817033	0.0589742	0.0210562	0	0
0.00424264	0.00515905	21213.6	598.563	0.835335	0.0597679	0.022071	0	0
0.00424264	0.0055559	19733.8	585.712	0.853662	0.0605616	0.0228763	0	0
0.00424264	0.00595275	18570.	573.388	0.87201	0.0613553	0.0235419	0	0
0.00424264	0.0063496	17645.9	561.56	0.890377	0.062149	0.0241085	0	0
0.00424264	0.00674645	16909.1	550.202	0.908756	0.0629427	0.0246019	0	0
0.00424264	0.0071433	16322.4	539.29	0.927146	0.0637364	0.0250395	0	0
0.00424264	0.00793701	15496.4	518.706	0.963937	0.0653238	0.025792	0	0
0.00459619	0.0039685	29305.8	640.596	0.780523	0.0580939	0.0176679	0	0
0.00459619	0.0047622	23129.1	611.97	0.817033	0.0596813	0.0210562	0	0
0.00459619	0.00515905	21213.6	598.563	0.835335	0.060475	0.022071	0	0
0.00459619	0.0055559	19733.8	585.712	0.853662	0.0612687	0.0228763	0	0
0.00459619	0.00595275	18570.	573.388	0.87201	0.0620624	0.0235419	0	0
0.00459619	0.0063496	17645.9	561.56	0.890377	0.0628561	0.0241085	0	0
0.00459619	0.00674645	16909.1	550.202	0.908756	0.0636498	0.0246019	0	0
0.00459619	0.0071433	16322.4	539.29	0.927146	0.0644435	0.0250395	0	0
0.00459619	0.00793701	15496.4	518.706	0.963937	0.0660309	0.025792	0	0
0.00494975	0.0039685	29305.8	640.596	0.780523	0.058801	0.0176679	0	0
0.00494975	0.0047622	23129.1	611.97	0.817033	0.0603884	0.0210562	0	0
0.00494975	0.00515905	21213.6	598.563	0.835335	0.0611821	0.022071	0	0
0.00494975	0.0055559	19733.8	585.712	0.853662	0.0619758	0.0228763	0	0
0.00494975	0.00595275	18570.	573.388	0.87201	0.0627695	0.0235419	0	0
0.00494975	0.0063496	17645.9	561.56	0.890377	0.0635632	0.0241085	0	0
0.00494975	0.00674645	16909.1	550.202	0.908756	0.0643569	0.0246019	0	0
0.00494975	0.0071433	16322.4	539.29	0.927146	0.0651506	0.0250395	0	0
0.00494975	0.00793701	15496.4	518.706	0.963937	0.066738	0.025792	0	0
0.0053033	0.0039685	29305.8	640.596	0.780523	0.0595081	0.0176679	0	0
0.0053033	0.0047622	23129.1	611.97	0.817033	0.0610955	0.0210562	0	0
0.0053033	0.00515905	21213.6	598.563	0.835335	0.0618892	0.022071	0	0
0.0053033	0.0055559	19733.8	585.712	0.853662	0.0626829	0.0228763	0	0
0.0053033	0.00595275	18570.	573.388	0.87201	0.0634766	0.0235419	0	0
0.0053033	0.0063496	17645.9	561.56	0.890377	0.0642703	0.0241085	0	0
0.0053033	0.00674645	16909.1	550.202	0.908756	0.065064	0.0246019	0	0
0.0053033	0.0071433	16322.4	539.29	0.927146	0.0658577	0.0250395	0	0
0.0053033	0.00793701	15496.4	518.706	0.963937	0.0674451	0.025792	0	0
0.00565685	0.0039685	29305.8	640.596	0.780523	0.0602152	0.0176679	0	0
0.00565685	0.0047622	23129.1	611.97	0.817033	0.0618026	0.0210562	0	0
0.00565685	0.00515905	21213.6	598.563	0.835335	0.0625963	0.022071	0	0
0.00565685	0.0055559	19733.8	585.712	0.853662	0.06339	0.0228763	0	0
0.00565685	0.00595275	18570.	573.388	0.87201	0.0641837	0.0235419	0	0
0.00565685	0.0063496	17645.9	561.56	0.890377	0.0649774	0.0241085	0	0
0.00565685	0.00674645	16909.1	550.202	0.908756	0.0657711	0.0246019	0	0
0.00565685	0.0071433	16322.4	539.29	0.927146	0.0665648	0.0250395	0	0
0.00565685	0.00793701	15496.4	518.706	0.963937	0.0681522	0.025792	0	0
0.00601041	0.0039685	29305.8	640.596	0.780523	0.0609223	0.0176679	0	0
0.00601041	0.0047622	23129.1	611.97	0.817033	0.0625097	0.0210562	0	0
0.00601041	0.00515905	21213.6	598.563	0.835335	0.0633034	0.022071	0	0
0.00601041	0.0055559	19733.8	585.712	0.853662	0.0640971	0.0228763	0	0
0.00601041	0.00595275	18570.	573.388	0.87201	0.0648908	0.0235419	0	0
0.00601041	0.0063496	17645.9	561.56	0.890377	0.0656845	0.0241085	0	0
0.00601041	0.00674645	16909.1	550.202	0.908756	0.0664782	0.0246019	0	0
0.00601041	0.0071433	16322.4	539.29	0.927146	0.0672719	0.0250395	0	0
0.00601041	0.00793701	15496.4	518.706	0.963937	0.0688593	0.025792	0	0
0.00636396	0.0039685	29305.8	640.596	0.780523	0.0616294	0.0176679	0	0
0.00636396	0.0047622	23129.1	611.97	0.817033	0.0632168	0.0210562	0	0
0.00636396	0.00515905	21213.6	598.563	0.835335	0.0640105	0.022071	0	0
0.00636396	0.0055559	19733.8	585.712	0.853662	0.0648042	0.0228763	0	0
0.00636396	0.00595275	18570.	573.388	0.87201	0.0655979	0.0235419	0	0
0.00636396	0.0063496	17645.9	561.56	0.890377	0.0663916	0.0241085	0	0
0.00636396	0.00674645	16909.1	550.202	0.908756	0.0671853	0.0246019	0	0
0.00636396	0.0071433	16322.4	539.29	0.927146	0.067979	0.0250395	0	0
0.00636396	0.00793701	15496.4	518.706	0.963937	0.0695664	0.025792	0	0
0.00707107	0.0039685	29305.8	640.596	0.780523	0.0630436	0.0176679	0	0
0.00707107	0.0047622	23129.1	611.97	0.817033	0.064631	0.0210562	0	0
0.00707107	0.00515905	21213.6	598.563	0.835335	0.0654247	0.022071	0	0
0.00707107	0.0055559	19733.8	585.712	0.853662	0.0662184	0.0228763	0	0
0.00707107	0.00595275	18570.	573.388	0.87201	0.0670121	0.0235419	0	0
0.00707107	0.0063496	17645.9	561.56	0.890377	0.0678058	0.0241085	0	0
0.00707107	0.00674645	16909.1	550.202	0.908756	0.0685995	0.0246019	0	0
0.00707107	0.0071433	16322.4	539.29	0.927146	0.0693932	0.0250395	0	0
0.00707107	0.00793701	15496.4	518.706	0.963937	0.0709806	0.025792	0	0

$RowBox[{aluminum, , thrust = , , 1000, , vol in^3 = , , 3.29466}]$

rBot	Wall	stress lbf	sp thrust	weight	dia	r max stress	min # noz	max # noz
0.005	0.005	29305.8	901.036	1.10983	0.071612	0.0222602	0	0
0.005	0.006	23129.1	861.876	1.16026	0.073612	0.0265291	0	0
0.005	0.0065	21213.6	843.615	1.18537	0.074612	0.0278078	0	0
0.005	0.007	19733.8	826.164	1.21041	0.075612	0.0288223	0	0
0.005	0.0075	18570.	809.476	1.23537	0.076612	0.0296609	0	0
0.005	0.008	17645.9	793.507	1.26023	0.077612	0.0303747	0	0
0.005	0.0085	16909.1	778.217	1.28499	0.078612	0.0309964	0	0
0.005	0.009	16322.4	763.569	1.30964	0.079612	0.0315477	0	0
0.005	0.01	15496.4	736.06	1.35859	0.081612	0.0324958	0	0
0.006	0.005	29305.8	901.036	1.10983	0.073612	0.0222602	0	0
0.006	0.006	23129.1	861.876	1.16026	0.075612	0.0265291	0	0
0.006	0.0065	21213.6	843.615	1.18537	0.076612	0.0278078	0	0
0.006	0.007	19733.8	826.164	1.21041	0.077612	0.0288223	0	0
0.006	0.0075	18570.	809.476	1.23537	0.078612	0.0296609	0	0
0.006	0.008	17645.9	793.507	1.26023	0.079612	0.0303747	0	0
0.006	0.0085	16909.1	778.217	1.28499	0.080612	0.0309964	0	0
0.006	0.009	16322.4	763.569	1.30964	0.081612	0.0315477	0	0
0.006	0.01	15496.4	736.06	1.35859	0.083612	0.0324958	0	0
0.0065	0.005	29305.8	901.036	1.10983	0.074612	0.0222602	0	0
0.0065	0.006	23129.1	861.876	1.16026	0.076612	0.0265291	0	0
0.0065	0.0065	21213.6	843.615	1.18537	0.077612	0.0278078	0	0
0.0065	0.007	19733.8	826.164	1.21041	0.078612	0.0288223	0	0
0.0065	0.0075	18570.	809.476	1.23537	0.079612	0.0296609	0	0
0.0065	0.008	17645.9	793.507	1.26023	0.080612	0.0303747	0	0
0.0065	0.0085	16909.1	778.217	1.28499	0.081612	0.0309964	0	0
0.0065	0.009	16322.4	763.569	1.30964	0.082612	0.0315477	0	0
0.0065	0.01	15496.4	736.06	1.35859	0.084612	0.0324958	0	0
0.007	0.005	29305.8	901.036	1.10983	0.075612	0.0222602	0	0
0.007	0.006	23129.1	861.876	1.16026	0.077612	0.0265291	0	0
0.007	0.0065	21213.6	843.615	1.18537	0.078612	0.0278078	0	0
0.007	0.007	19733.8	826.164	1.21041	0.079612	0.0288223	0	0
0.007	0.0075	18570.	809.476	1.23537	0.080612	0.0296609	0	0
0.007	0.008	17645.9	793.507	1.26023	0.081612	0.0303747	0	0
0.007	0.0085	16909.1	778.217	1.28499	0.082612	0.0309964	0	0
0.007	0.009	16322.4	763.569	1.30964	0.083612	0.0315477	0	0
0.007	0.01	15496.4	736.06	1.35859	0.085612	0.0324958	0	0
0.0075	0.005	29305.8	901.036	1.10983	0.076612	0.0222602	0	0
0.0075	0.006	23129.1	861.876	1.16026	0.078612	0.0265291	0	0
0.0075	0.0065	21213.6	843.615	1.18537	0.079612	0.0278078	0	0
0.0075	0.007	19733.8	826.164	1.21041	0.080612	0.0288223	0	0
0.0075	0.0075	18570.	809.476	1.23537	0.081612	0.0296609	0	0
0.0075	0.008	17645.9	793.507	1.26023	0.082612	0.0303747	0	0
0.0075	0.0085	16909.1	778.217	1.28499	0.083612	0.0309964	0	0
0.0075	0.009	16322.4	763.569	1.30964	0.084612	0.0315477	0	0
0.0075	0.01	15496.4	736.06	1.35859	0.086612	0.0324958	0	0
0.008	0.005	29305.8	901.036	1.10983	0.077612	0.0222602	0	0
0.008	0.006	23129.1	861.876	1.16026	0.079612	0.0265291	0	0
0.008	0.0065	21213.6	843.615	1.18537	0.080612	0.0278078	0	0
0.008	0.007	19733.8	826.164	1.21041	0.081612	0.0288223	0	0
0.008	0.0075	18570.	809.476	1.23537	0.082612	0.0296609	0	0
0.008	0.008	17645.9	793.507	1.26023	0.083612	0.0303747	0	0
0.008	0.0085	16909.1	778.217	1.28499	0.084612	0.0309964	0	0
0.008	0.009	16322.4	763.569	1.30964	0.085612	0.0315477	0	0
0.008	0.01	15496.4	736.06	1.35859	0.087612	0.0324958	0	0
0.0085	0.005	29305.8	901.036	1.10983	0.078612	0.0222602	0	0
0.0085	0.006	23129.1	861.876	1.16026	0.080612	0.0265291	0	0
0.0085	0.0065	21213.6	843.615	1.18537	0.081612	0.0278078	0	0
0.0085	0.007	19733.8	826.164	1.21041	0.082612	0.0288223	0	0
0.0085	0.0075	18570.	809.476	1.23537	0.083612	0.0296609	0	0
0.0085	0.008	17645.9	793.507	1.26023	0.084612	0.0303747	0	0
0.0085	0.0085	16909.1	778.217	1.28499	0.085612	0.0309964	0	0
0.0085	0.009	16322.4	763.569	1.30964	0.086612	0.0315477	0	0
0.0085	0.01	15496.4	736.06	1.35859	0.088612	0.0324958	0	0
0.009	0.005	29305.8	901.036	1.10983	0.079612	0.0222602	0	0
0.009	0.006	23129.1	861.876	1.16026	0.081612	0.0265291	0	0
0.009	0.0065	21213.6	843.615	1.18537	0.082612	0.0278078	0	0
0.009	0.007	19733.8	826.164	1.21041	0.083612	0.0288223	0	0
0.009	0.0075	18570.	809.476	1.23537	0.084612	0.0296609	0	0
0.009	0.008	17645.9	793.507	1.26023	0.085612	0.0303747	0	0
0.009	0.0085	16909.1	778.217	1.28499	0.086612	0.0309964	0	0
0.009	0.009	16322.4	763.569	1.30964	0.087612	0.0315477	0	0
0.009	0.01	15496.4	736.06	1.35859	0.089612	0.0324958	0	0
0.01	0.005	29305.8	901.036	1.10983	0.081612	0.0222602	0	0
0.01	0.006	23129.1	861.876	1.16026	0.083612	0.0265291	0	0
0.01	0.0065	21213.6	843.615	1.18537	0.084612	0.0278078	0	0
0.01	0.007	19733.8	826.164	1.21041	0.085612	0.0288223	0	0
0.01	0.0075	18570.	809.476	1.23537	0.086612	0.0296609	0	0
0.01	0.008	17645.9	793.507	1.26023	0.087612	0.0303747	0	0
0.01	0.0085	16909.1	778.217	1.28499	0.088612	0.0309964	0	0
0.01	0.009	16322.4	763.569	1.30964	0.089612	0.0315477	0	0
0.01	0.01	15496.4	736.06	1.35859	0.091612	0.0324958	0	0

$RowBox[{stainlesssteel420, , thrust = , , 100, , vol in^3 = , , 0.329466}]$

rBot	Wall	stress lbf	sp thrust	weight	dia	r max stress	min # noz	max # noz
0.00158114	0.000464159	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	146.447	0.682843	0.0280468	RowBox[{RowBox[{0.010485, }], +, RowBox[{0.010485, , i}]}]	0	0
0.00158114	0.00232079	33313.	118.498	0.843893	0.03176	0.0143017	0	0
0.00158114	0.00348119	27934.7	105.346	0.949253	0.0340808	0.0153235	0	0
0.00158114	0.00464159	27997.9	94.5269	1.0579	0.0364016	0.0160003	0	0
0.00158114	0.011604	56789.9	56.7135	1.76325	0.0503264	0.0187189	0	0
0.00158114	0.0139248	71726.6	49.6999	2.01208	0.054968	0.0194716	0	0
0.00158114	0.0185664	107788.	39.7299	2.517	0.0642512	0.0208759	0	0
0.00158114	0.0208871	128798.	36.1187	2.76865	0.0688927	0.0215388	0	0
0.00158114	0.0232079	151760.	33.1477	3.0168	0.0735343	0.0221801	0	0
0.00158114	0.0255287	176661.	30.682	3.25924	0.0781759	0.0228021	0	0
0.00158114	0.0278495	203492.	28.6226	3.49375	0.0828175	0.0234069	0	0
0.00158114	0.0348119	295522.	24.2279	4.12747	0.0967423	0.025131	0	0
0.00158114	0.0464159	487231.	20.7559	4.8179	0.11995	0.0277634	0	0
0.00189737	0.000464159	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	146.447	0.682843	0.0286792	RowBox[{RowBox[{0.010485, }], +, RowBox[{0.010485, , i}]}]	0	0
0.00189737	0.00232079	33313.	118.498	0.843893	0.0323925	0.0143017	0	0
0.00189737	0.00348119	27934.7	105.346	0.949253	0.0347133	0.0153235	0	0
0.00189737	0.00464159	27997.9	94.5269	1.0579	0.0370341	0.0160003	0	0
0.00189737	0.011604	56789.9	56.7135	1.76325	0.0509588	0.0187189	0	0
0.00189737	0.0139248	71726.6	49.6999	2.01208	0.0556004	0.0194716	0	0
0.00189737	0.0185664	107788.	39.7299	2.517	0.0648836	0.0208759	0	0
0.00189737	0.0208871	128798.	36.1187	2.76865	0.0695252	0.0215388	0	0
0.00189737	0.0232079	151760.	33.1477	3.0168	0.0741668	0.0221801	0	0
0.00189737	0.0255287	176661.	30.682	3.25924	0.0788084	0.0228021	0	0
0.00189737	0.0278495	203492.	28.6226	3.49375	0.08345	0.0234069	0	0
0.00189737	0.0348119	295522.	24.2279	4.12747	0.0973747	0.025131	0	0
0.00189737	0.0464159	487231.	20.7559	4.8179	0.120583	0.0277634	0	0
0.00205548	0.000464159	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	146.447	0.682843	0.0289955	RowBox[{RowBox[{0.010485, }], +, RowBox[{0.010485, , i}]}]	0	0
0.00205548	0.00232079	33313.	118.498	0.843893	0.0327087	0.0143017	0	0
0.00205548	0.00348119	27934.7	105.346	0.949253	0.0350295	0.0153235	0	0
0.00205548	0.00464159	27997.9	94.5269	1.0579	0.0373503	0.0160003	0	0
0.00205548	0.011604	56789.9	56.7135	1.76325	0.0512751	0.0187189	0	0
0.00205548	0.0139248	71726.6	49.6999	2.01208	0.0559167	0.0194716	0	0
0.00205548	0.0185664	107788.	39.7299	2.517	0.0651998	0.0208759	0	0
0.00205548	0.0208871	128798.	36.1187	2.76865	0.0698414	0.0215388	0	0
0.00205548	0.0232079	151760.	33.1477	3.0168	0.074483	0.0221801	0	0
0.00205548	0.0255287	176661.	30.682	3.25924	0.0791246	0.0228021	0	0
0.00205548	0.0278495	203492.	28.6226	3.49375	0.0837662	0.0234069	0	0
0.00205548	0.0348119	295522.	24.2279	4.12747	0.097691	0.025131	0	0
0.00205548	0.0464159	487231.	20.7559	4.8179	0.120899	0.0277634	0	0
0.00221359	0.000464159	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	146.447	0.682843	0.0293117	RowBox[{RowBox[{0.010485, }], +, RowBox[{0.010485, , i}]}]	0	0
0.00221359	0.00232079	33313.	118.498	0.843893	0.0330249	0.0143017	0	0
0.00221359	0.00348119	27934.7	105.346	0.949253	0.0353457	0.0153235	0	0
0.00221359	0.00464159	27997.9	94.5269	1.0579	0.0376665	0.0160003	0	0
0.00221359	0.011604	56789.9	56.7135	1.76325	0.0515913	0.0187189	0	0
0.00221359	0.0139248	71726.6	49.6999	2.01208	0.0562329	0.0194716	0	0
0.00221359	0.0185664	107788.	39.7299	2.517	0.0655161	0.0208759	0	0
0.00221359	0.0208871	128798.	36.1187	2.76865	0.0701577	0.0215388	0	0
0.00221359	0.0232079	151760.	33.1477	3.0168	0.0747992	0.0221801	0	0
0.00221359	0.0255287	176661.	30.682	3.25924	0.0794408	0.0228021	0	0
0.00221359	0.0278495	203492.	28.6226	3.49375	0.0840824	0.0234069	0	0
0.00221359	0.0348119	295522.	24.2279	4.12747	0.0980072	0.025131	0	0
0.00221359	0.0464159	487231.	20.7559	4.8179	0.121215	0.0277634	0	0
0.00237171	0.000464159	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	146.447	0.682843	0.0296279	RowBox[{RowBox[{0.010485, }], +, RowBox[{0.010485, , i}]}]	0	0
0.00237171	0.00232079	33313.	118.498	0.843893	0.0333412	0.0143017	0	0
0.00237171	0.00348119	27934.7	105.346	0.949253	0.035662	0.0153235	0	0
0.00237171	0.00464159	27997.9	94.5269	1.0579	0.0379828	0.0160003	0	0
0.00237171	0.011604	56789.9	56.7135	1.76325	0.0519075	0.0187189	0	0
0.00237171	0.0139248	71726.6	49.6999	2.01208	0.0565491	0.0194716	0	0
0.00237171	0.0185664	107788.	39.7299	2.517	0.0658323	0.0208759	0	0
0.00237171	0.0208871	128798.	36.1187	2.76865	0.0704739	0.0215388	0	0
0.00237171	0.0232079	151760.	33.1477	3.0168	0.0751155	0.0221801	0	0
0.00237171	0.0255287	176661.	30.682	3.25924	0.0797571	0.0228021	0	0
0.00237171	0.0278495	203492.	28.6226	3.49375	0.0843987	0.0234069	0	0
0.00237171	0.0348119	295522.	24.2279	4.12747	0.0983234	0.025131	0	0
0.00237171	0.0464159	487231.	20.7559	4.8179	0.121531	0.0277634	0	0
0.00252982	0.000464159	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	146.447	0.682843	0.0299441	RowBox[{RowBox[{0.010485, }], +, RowBox[{0.010485, , i}]}]	0	0
0.00252982	0.00232079	33313.	118.498	0.843893	0.0336574	0.0143017	0	0
0.00252982	0.00348119	27934.7	105.346	0.949253	0.0359782	0.0153235	0	0
0.00252982	0.00464159	27997.9	94.5269	1.0579	0.038299	0.0160003	0	0
0.00252982	0.011604	56789.9	56.7135	1.76325	0.0522238	0.0187189	0	0
0.00252982	0.0139248	71726.6	49.6999	2.01208	0.0568653	0.0194716	0	0
0.00252982	0.0185664	107788.	39.7299	2.517	0.0661485	0.0208759	0	0
0.00252982	0.0208871	128798.	36.1187	2.76865	0.0707901	0.0215388	0	0
0.00252982	0.0232079	151760.	33.1477	3.0168	0.0754317	0.0221801	0	0
0.00252982	0.0255287	176661.	30.682	3.25924	0.0800733	0.0228021	0	0
0.00252982	0.0278495	203492.	28.6226	3.49375	0.0847149	0.0234069	0	0
0.00252982	0.0348119	295522.	24.2279	4.12747	0.0986396	0.025131	0	0
0.00252982	0.0464159	487231.	20.7559	4.8179	0.121848	0.0277634	0	0
0.00268794	0.000464159	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	146.447	0.682843	0.0302604	RowBox[{RowBox[{0.010485, }], +, RowBox[{0.010485, , i}]}]	0	0
0.00268794	0.00232079	33313.	118.498	0.843893	0.0339736	0.0143017	0	0
0.00268794	0.00348119	27934.7	105.346	0.949253	0.0362944	0.0153235	0	0
0.00268794	0.00464159	27997.9	94.5269	1.0579	0.0386152	0.0160003	0	0
0.00268794	0.011604	56789.9	56.7135	1.76325	0.05254	0.0187189	0	0
0.00268794	0.0139248	71726.6	49.6999	2.01208	0.0571816	0.0194716	0	0
0.00268794	0.0185664	107788.	39.7299	2.517	0.0664648	0.0208759	0	0
0.00268794	0.0208871	128798.	36.1187	2.76865	0.0711063	0.0215388	0	0
0.00268794	0.0232079	151760.	33.1477	3.0168	0.0757479	0.0221801	0	0
0.00268794	0.0255287	176661.	30.682	3.25924	0.0803895	0.0228021	0	0
0.00268794	0.0278495	203492.	28.6226	3.49375	0.0850311	0.0234069	0	0
0.00268794	0.0348119	295522.	24.2279	4.12747	0.0989559	0.025131	0	0
0.00268794	0.0464159	487231.	20.7559	4.8179	0.122164	0.0277634	0	0
0.00284605	0.000464159	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	146.447	0.682843	0.0305766	RowBox[{RowBox[{0.010485, }], +, RowBox[{0.010485, , i}]}]	0	0
0.00284605	0.00232079	33313.	118.498	0.843893	0.0342899	0.0143017	0	0
0.00284605	0.00348119	27934.7	105.346	0.949253	0.0366107	0.0153235	0	0
0.00284605	0.00464159	27997.9	94.5269	1.0579	0.0389314	0.0160003	0	0
0.00284605	0.011604	56789.9	56.7135	1.76325	0.0528562	0.0187189	0	0
0.00284605	0.0139248	71726.6	49.6999	2.01208	0.0574978	0.0194716	0	0
0.00284605	0.0185664	107788.	39.7299	2.517	0.066781	0.0208759	0	0
0.00284605	0.0208871	128798.	36.1187	2.76865	0.0714226	0.0215388	0	0
0.00284605	0.0232079	151760.	33.1477	3.0168	0.0760642	0.0221801	0	0
0.00284605	0.0255287	176661.	30.682	3.25924	0.0807057	0.0228021	0	0
0.00284605	0.0278495	203492.	28.6226	3.49375	0.0853473	0.0234069	0	0
0.00284605	0.0348119	295522.	24.2279	4.12747	0.0992721	0.025131	0	0
0.00284605	0.0464159	487231.	20.7559	4.8179	0.12248	0.0277634	0	0
0.00316228	0.000464159	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	146.447	0.682843	0.031209	RowBox[{RowBox[{0.010485, }], +, RowBox[{0.010485, , i}]}]	0	0
0.00316228	0.00232079	33313.	118.498	0.843893	0.0349223	0.0143017	0	0
0.00316228	0.00348119	27934.7	105.346	0.949253	0.0372431	0.0153235	0	0
0.00316228	0.00464159	27997.9	94.5269	1.0579	0.0395639	0.0160003	0	0
0.00316228	0.011604	56789.9	56.7135	1.76325	0.0534887	0.0187189	0	0
0.00316228	0.0139248	71726.6	49.6999	2.01208	0.0581303	0.0194716	0	0
0.00316228	0.0185664	107788.	39.7299	2.517	0.0674134	0.0208759	0	0
0.00316228	0.0208871	128798.	36.1187	2.76865	0.072055	0.0215388	0	0
0.00316228	0.0232079	151760.	33.1477	3.0168	0.0766966	0.0221801	0	0
0.00316228	0.0255287	176661.	30.682	3.25924	0.0813382	0.0228021	0	0
0.00316228	0.0278495	203492.	28.6226	3.49375	0.0859798	0.0234069	0	0
0.00316228	0.0348119	295522.	24.2279	4.12747	0.0999046	0.025131	0	0
0.00316228	0.0464159	487231.	20.7559	4.8179	0.123113	0.0277634	0	0

$RowBox[{stainlesssteel420, , thrust = , , 1000, , vol in^3 = , , 3.29466}]$

rBot	Wall	stress lbf	sp thrust	weight	dia	r max stress	min # noz	max # noz
0.005	0.001	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	398.483	2.50952	0.063612	RowBox[{RowBox[{0.0225893, }], +, RowBox[{0.0225893, , i}]}]	0	0
0.005	0.005	33313.	325.536	3.07186	0.071612	0.0308121	0	0
0.005	0.0075	27934.7	292.456	3.41932	0.076612	0.0330136	0	0
0.005	0.01	27997.9	265.931	3.76037	0.081612	0.0344716	0	0
0.005	0.025	56789.9	181.264	5.5168	0.111612	0.0403286	0	0
0.005	0.03	71726.6	168.768	5.92529	0.121612	0.0419504	0	0
0.005	0.04	107788.	157.638	6.34366	0.141612	0.0449757	0	0
0.005	0.045	128798.	158.5	6.30917	0.151612	0.0464038	0	0
0.005	0.05	151760.	164.402	6.08264	0.161612	0.0477855	0	0
0.005	0.055	176661.	177.246	5.64189	0.171612	0.0491257	0	0
0.005	0.06	203492.	201.421	4.96474	0.181612	0.0504286	0	0
0.005	0.075	295522.	773.427	1.29295	0.211612	0.0541431	0	0
0.005	0.1	487231.	RowBox[{-, 86.0167}]	RowBox[{-, 11.6256}]	0.261612	0.0598145	0	0
0.006	0.001	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	398.483	2.50952	0.065612	RowBox[{RowBox[{0.0225893, }], +, RowBox[{0.0225893, , i}]}]	0	0
0.006	0.005	33313.	325.536	3.07186	0.073612	0.0308121	0	0
0.006	0.0075	27934.7	292.456	3.41932	0.078612	0.0330136	0	0
0.006	0.01	27997.9	265.931	3.76037	0.083612	0.0344716	0	0
0.006	0.025	56789.9	181.264	5.5168	0.113612	0.0403286	0	0
0.006	0.03	71726.6	168.768	5.92529	0.123612	0.0419504	0	0
0.006	0.04	107788.	157.638	6.34366	0.143612	0.0449757	0	0
0.006	0.045	128798.	158.5	6.30917	0.153612	0.0464038	0	0
0.006	0.05	151760.	164.402	6.08264	0.163612	0.0477855	0	0
0.006	0.055	176661.	177.246	5.64189	0.173612	0.0491257	0	0
0.006	0.06	203492.	201.421	4.96474	0.183612	0.0504286	0	0
0.006	0.075	295522.	773.427	1.29295	0.213612	0.0541431	0	0
0.006	0.1	487231.	RowBox[{-, 86.0167}]	RowBox[{-, 11.6256}]	0.263612	0.0598145	0	0
0.0065	0.001	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	398.483	2.50952	0.066612	RowBox[{RowBox[{0.0225893, }], +, RowBox[{0.0225893, , i}]}]	0	0
0.0065	0.005	33313.	325.536	3.07186	0.074612	0.0308121	0	0
0.0065	0.0075	27934.7	292.456	3.41932	0.079612	0.0330136	0	0
0.0065	0.01	27997.9	265.931	3.76037	0.084612	0.0344716	0	0
0.0065	0.025	56789.9	181.264	5.5168	0.114612	0.0403286	0	0
0.0065	0.03	71726.6	168.768	5.92529	0.124612	0.0419504	0	0
0.0065	0.04	107788.	157.638	6.34366	0.144612	0.0449757	0	0
0.0065	0.045	128798.	158.5	6.30917	0.154612	0.0464038	0	0
0.0065	0.05	151760.	164.402	6.08264	0.164612	0.0477855	0	0
0.0065	0.055	176661.	177.246	5.64189	0.174612	0.0491257	0	0
0.0065	0.06	203492.	201.421	4.96474	0.184612	0.0504286	0	0
0.0065	0.075	295522.	773.427	1.29295	0.214612	0.0541431	0	0
0.0065	0.1	487231.	RowBox[{-, 86.0167}]	RowBox[{-, 11.6256}]	0.264612	0.0598145	0	0
0.007	0.001	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	398.483	2.50952	0.067612	RowBox[{RowBox[{0.0225893, }], +, RowBox[{0.0225893, , i}]}]	0	0
0.007	0.005	33313.	325.536	3.07186	0.075612	0.0308121	0	0
0.007	0.0075	27934.7	292.456	3.41932	0.080612	0.0330136	0	0
0.007	0.01	27997.9	265.931	3.76037	0.085612	0.0344716	0	0
0.007	0.025	56789.9	181.264	5.5168	0.115612	0.0403286	0	0
0.007	0.03	71726.6	168.768	5.92529	0.125612	0.0419504	0	0
0.007	0.04	107788.	157.638	6.34366	0.145612	0.0449757	0	0
0.007	0.045	128798.	158.5	6.30917	0.155612	0.0464038	0	0
0.007	0.05	151760.	164.402	6.08264	0.165612	0.0477855	0	0
0.007	0.055	176661.	177.246	5.64189	0.175612	0.0491257	0	0
0.007	0.06	203492.	201.421	4.96474	0.185612	0.0504286	0	0
0.007	0.075	295522.	773.427	1.29295	0.215612	0.0541431	0	0
0.007	0.1	487231.	RowBox[{-, 86.0167}]	RowBox[{-, 11.6256}]	0.265612	0.0598145	0	0
0.0075	0.001	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	398.483	2.50952	0.068612	RowBox[{RowBox[{0.0225893, }], +, RowBox[{0.0225893, , i}]}]	0	0
0.0075	0.005	33313.	325.536	3.07186	0.076612	0.0308121	0	0
0.0075	0.0075	27934.7	292.456	3.41932	0.081612	0.0330136	0	0
0.0075	0.01	27997.9	265.931	3.76037	0.086612	0.0344716	0	0
0.0075	0.025	56789.9	181.264	5.5168	0.116612	0.0403286	0	0
0.0075	0.03	71726.6	168.768	5.92529	0.126612	0.0419504	0	0
0.0075	0.04	107788.	157.638	6.34366	0.146612	0.0449757	0	0
0.0075	0.045	128798.	158.5	6.30917	0.156612	0.0464038	0	0
0.0075	0.05	151760.	164.402	6.08264	0.166612	0.0477855	0	0
0.0075	0.055	176661.	177.246	5.64189	0.176612	0.0491257	0	0
0.0075	0.06	203492.	201.421	4.96474	0.186612	0.0504286	0	0
0.0075	0.075	295522.	773.427	1.29295	0.216612	0.0541431	0	0
0.0075	0.1	487231.	RowBox[{-, 86.0167}]	RowBox[{-, 11.6256}]	0.266612	0.0598145	0	0
0.008	0.001	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	398.483	2.50952	0.069612	RowBox[{RowBox[{0.0225893, }], +, RowBox[{0.0225893, , i}]}]	0	0
0.008	0.005	33313.	325.536	3.07186	0.077612	0.0308121	0	0
0.008	0.0075	27934.7	292.456	3.41932	0.082612	0.0330136	0	0
0.008	0.01	27997.9	265.931	3.76037	0.087612	0.0344716	0	0
0.008	0.025	56789.9	181.264	5.5168	0.117612	0.0403286	0	0
0.008	0.03	71726.6	168.768	5.92529	0.127612	0.0419504	0	0
0.008	0.04	107788.	157.638	6.34366	0.147612	0.0449757	0	0
0.008	0.045	128798.	158.5	6.30917	0.157612	0.0464038	0	0
0.008	0.05	151760.	164.402	6.08264	0.167612	0.0477855	0	0
0.008	0.055	176661.	177.246	5.64189	0.177612	0.0491257	0	0
0.008	0.06	203492.	201.421	4.96474	0.187612	0.0504286	0	0
0.008	0.075	295522.	773.427	1.29295	0.217612	0.0541431	0	0
0.008	0.1	487231.	RowBox[{-, 86.0167}]	RowBox[{-, 11.6256}]	0.267612	0.0598145	0	0
0.0085	0.001	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	398.483	2.50952	0.070612	RowBox[{RowBox[{0.0225893, }], +, RowBox[{0.0225893, , i}]}]	0	0
0.0085	0.005	33313.	325.536	3.07186	0.078612	0.0308121	0	0
0.0085	0.0075	27934.7	292.456	3.41932	0.083612	0.0330136	0	0
0.0085	0.01	27997.9	265.931	3.76037	0.088612	0.0344716	0	0
0.0085	0.025	56789.9	181.264	5.5168	0.118612	0.0403286	0	0
0.0085	0.03	71726.6	168.768	5.92529	0.128612	0.0419504	0	0
0.0085	0.04	107788.	157.638	6.34366	0.148612	0.0449757	0	0
0.0085	0.045	128798.	158.5	6.30917	0.158612	0.0464038	0	0
0.0085	0.05	151760.	164.402	6.08264	0.168612	0.0477855	0	0
0.0085	0.055	176661.	177.246	5.64189	0.178612	0.0491257	0	0
0.0085	0.06	203492.	201.421	4.96474	0.188612	0.0504286	0	0
0.0085	0.075	295522.	773.427	1.29295	0.218612	0.0541431	0	0
0.0085	0.1	487231.	RowBox[{-, 86.0167}]	RowBox[{-, 11.6256}]	0.268612	0.0598145	0	0
0.009	0.001	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	398.483	2.50952	0.071612	RowBox[{RowBox[{0.0225893, }], +, RowBox[{0.0225893, , i}]}]	0	0
0.009	0.005	33313.	325.536	3.07186	0.079612	0.0308121	0	0
0.009	0.0075	27934.7	292.456	3.41932	0.084612	0.0330136	0	0
0.009	0.01	27997.9	265.931	3.76037	0.089612	0.0344716	0	0
0.009	0.025	56789.9	181.264	5.5168	0.119612	0.0403286	0	0
0.009	0.03	71726.6	168.768	5.92529	0.129612	0.0419504	0	0
0.009	0.04	107788.	157.638	6.34366	0.149612	0.0449757	0	0
0.009	0.045	128798.	158.5	6.30917	0.159612	0.0464038	0	0
0.009	0.05	151760.	164.402	6.08264	0.169612	0.0477855	0	0
0.009	0.055	176661.	177.246	5.64189	0.179612	0.0491257	0	0
0.009	0.06	203492.	201.421	4.96474	0.189612	0.0504286	0	0
0.009	0.075	295522.	773.427	1.29295	0.219612	0.0541431	0	0
0.009	0.1	487231.	RowBox[{-, 86.0167}]	RowBox[{-, 11.6256}]	0.269612	0.0598145	0	0
0.01	0.001	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	398.483	2.50952	0.073612	RowBox[{RowBox[{0.0225893, }], +, RowBox[{0.0225893, , i}]}]	0	0
0.01	0.005	33313.	325.536	3.07186	0.081612	0.0308121	0	0
0.01	0.0075	27934.7	292.456	3.41932	0.086612	0.0330136	0	0
0.01	0.01	27997.9	265.931	3.76037	0.091612	0.0344716	0	0
0.01	0.025	56789.9	181.264	5.5168	0.121612	0.0403286	0	0
0.01	0.03	71726.6	168.768	5.92529	0.131612	0.0419504	0	0
0.01	0.04	107788.	157.638	6.34366	0.151612	0.0449757	0	0
0.01	0.045	128798.	158.5	6.30917	0.161612	0.0464038	0	0
0.01	0.05	151760.	164.402	6.08264	0.171612	0.0477855	0	0
0.01	0.055	176661.	177.246	5.64189	0.181612	0.0491257	0	0
0.01	0.06	203492.	201.421	4.96474	0.191612	0.0504286	0	0
0.01	0.075	295522.	773.427	1.29295	0.221612	0.0541431	0	0
0.01	0.1	487231.	RowBox[{-, 86.0167}]	RowBox[{-, 11.6256}]	0.271612	0.0598145	0	0

$RowBox[{stainlesssteel420, , thrust = , , 10000, , vol in^3 = , , 32.9466}]$

rBot	Wall	stress lbf	sp thrust	weight	dia	r max stress	min # noz	max # noz
0.0158114	0.00215443	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	2881.	3.47101	0.147126	RowBox[{RowBox[{0.0486673, }], +, RowBox[{0.0486673, , i}]}]	0	0
0.0158114	0.0107722	33313.	2364.46	4.2293	0.164362	0.0663826	0	0
0.0158114	0.0161583	27934.7	2259.24	4.42626	0.175134	0.0711255	0	0
0.0158114	0.0215443	27997.9	2284.73	4.37688	0.185906	0.0742669	0	0
0.0158114	0.0538609	56789.9	RowBox[{-, 3779.93}]	RowBox[{-, 2.64555}]	0.250539	0.0868854	0	0
0.0158114	0.064633	71726.6	RowBox[{-, 1217.39}]	RowBox[{-, 8.21431}]	0.272084	0.0903793	0	0
0.0158114	0.0861774	107788.	RowBox[{-, 391.773}]	RowBox[{-, 25.525}]	0.315172	0.0968973	0	0
0.0158114	0.0969496	128798.	RowBox[{-, 265.177}]	RowBox[{-, 37.7106}]	0.336717	0.099974	0	0
0.0158114	0.107722	151760.	RowBox[{-, 190.311}]	RowBox[{-, 52.5456}]	0.358261	0.102951	0	0
0.0158114	0.118494	176661.	RowBox[{-, 142.345}]	RowBox[{-, 70.2519}]	0.379805	0.105838	0	0
0.0158114	0.129266	203492.	RowBox[{-, 109.828}]	RowBox[{-, 91.0513}]	0.40135	0.108645	0	0
0.0158114	0.161583	295522.	RowBox[{-, 57.3965}]	RowBox[{-, 174.227}]	0.465983	0.116648	0	0
0.0158114	0.215443	487231.	RowBox[{-, 25.2894}]	RowBox[{-, 395.423}]	0.573704	0.128866	0	0
0.0189737	0.00215443	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	2881.	3.47101	0.153451	RowBox[{RowBox[{0.0486673, }], +, RowBox[{0.0486673, , i}]}]	0	0
0.0189737	0.0107722	33313.	2364.46	4.2293	0.170686	0.0663826	0	0
0.0189737	0.0161583	27934.7	2259.24	4.42626	0.181459	0.0711255	0	0
0.0189737	0.0215443	27997.9	2284.73	4.37688	0.192231	0.0742669	0	0
0.0189737	0.0538609	56789.9	RowBox[{-, 3779.93}]	RowBox[{-, 2.64555}]	0.256864	0.0868854	0	0
0.0189737	0.064633	71726.6	RowBox[{-, 1217.39}]	RowBox[{-, 8.21431}]	0.278408	0.0903793	0	0
0.0189737	0.0861774	107788.	RowBox[{-, 391.773}]	RowBox[{-, 25.525}]	0.321497	0.0968973	0	0
0.0189737	0.0969496	128798.	RowBox[{-, 265.177}]	RowBox[{-, 37.7106}]	0.343041	0.099974	0	0
0.0189737	0.107722	151760.	RowBox[{-, 190.311}]	RowBox[{-, 52.5456}]	0.364585	0.102951	0	0
0.0189737	0.118494	176661.	RowBox[{-, 142.345}]	RowBox[{-, 70.2519}]	0.38613	0.105838	0	0
0.0189737	0.129266	203492.	RowBox[{-, 109.828}]	RowBox[{-, 91.0513}]	0.407674	0.108645	0	0
0.0189737	0.161583	295522.	RowBox[{-, 57.3965}]	RowBox[{-, 174.227}]	0.472307	0.116648	0	0
0.0189737	0.215443	487231.	RowBox[{-, 25.2894}]	RowBox[{-, 395.423}]	0.580029	0.128866	0	0
0.0205548	0.00215443	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	2881.	3.47101	0.156613	RowBox[{RowBox[{0.0486673, }], +, RowBox[{0.0486673, , i}]}]	0	0
0.0205548	0.0107722	33313.	2364.46	4.2293	0.173849	0.0663826	0	0
0.0205548	0.0161583	27934.7	2259.24	4.42626	0.184621	0.0711255	0	0
0.0205548	0.0215443	27997.9	2284.73	4.37688	0.195393	0.0742669	0	0
0.0205548	0.0538609	56789.9	RowBox[{-, 3779.93}]	RowBox[{-, 2.64555}]	0.260026	0.0868854	0	0
0.0205548	0.064633	71726.6	RowBox[{-, 1217.39}]	RowBox[{-, 8.21431}]	0.28157	0.0903793	0	0
0.0205548	0.0861774	107788.	RowBox[{-, 391.773}]	RowBox[{-, 25.525}]	0.324659	0.0968973	0	0
0.0205548	0.0969496	128798.	RowBox[{-, 265.177}]	RowBox[{-, 37.7106}]	0.346203	0.099974	0	0
0.0205548	0.107722	151760.	RowBox[{-, 190.311}]	RowBox[{-, 52.5456}]	0.367748	0.102951	0	0
0.0205548	0.118494	176661.	RowBox[{-, 142.345}]	RowBox[{-, 70.2519}]	0.389292	0.105838	0	0
0.0205548	0.129266	203492.	RowBox[{-, 109.828}]	RowBox[{-, 91.0513}]	0.410836	0.108645	0	0
0.0205548	0.161583	295522.	RowBox[{-, 57.3965}]	RowBox[{-, 174.227}]	0.47547	0.116648	0	0
0.0205548	0.215443	487231.	RowBox[{-, 25.2894}]	RowBox[{-, 395.423}]	0.583191	0.128866	0	0
0.0221359	0.00215443	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	2881.	3.47101	0.159775	RowBox[{RowBox[{0.0486673, }], +, RowBox[{0.0486673, , i}]}]	0	0
0.0221359	0.0107722	33313.	2364.46	4.2293	0.177011	0.0663826	0	0
0.0221359	0.0161583	27934.7	2259.24	4.42626	0.187783	0.0711255	0	0
0.0221359	0.0215443	27997.9	2284.73	4.37688	0.198555	0.0742669	0	0
0.0221359	0.0538609	56789.9	RowBox[{-, 3779.93}]	RowBox[{-, 2.64555}]	0.263188	0.0868854	0	0
0.0221359	0.064633	71726.6	RowBox[{-, 1217.39}]	RowBox[{-, 8.21431}]	0.284733	0.0903793	0	0
0.0221359	0.0861774	107788.	RowBox[{-, 391.773}]	RowBox[{-, 25.525}]	0.327821	0.0968973	0	0
0.0221359	0.0969496	128798.	RowBox[{-, 265.177}]	RowBox[{-, 37.7106}]	0.349366	0.099974	0	0
0.0221359	0.107722	151760.	RowBox[{-, 190.311}]	RowBox[{-, 52.5456}]	0.37091	0.102951	0	0
0.0221359	0.118494	176661.	RowBox[{-, 142.345}]	RowBox[{-, 70.2519}]	0.392454	0.105838	0	0
0.0221359	0.129266	203492.	RowBox[{-, 109.828}]	RowBox[{-, 91.0513}]	0.413999	0.108645	0	0
0.0221359	0.161583	295522.	RowBox[{-, 57.3965}]	RowBox[{-, 174.227}]	0.478632	0.116648	0	0
0.0221359	0.215443	487231.	RowBox[{-, 25.2894}]	RowBox[{-, 395.423}]	0.586354	0.128866	0	0
0.0237171	0.00215443	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	2881.	3.47101	0.162938	RowBox[{RowBox[{0.0486673, }], +, RowBox[{0.0486673, , i}]}]	0	0
0.0237171	0.0107722	33313.	2364.46	4.2293	0.180173	0.0663826	0	0
0.0237171	0.0161583	27934.7	2259.24	4.42626	0.190945	0.0711255	0	0
0.0237171	0.0215443	27997.9	2284.73	4.37688	0.201718	0.0742669	0	0
0.0237171	0.0538609	56789.9	RowBox[{-, 3779.93}]	RowBox[{-, 2.64555}]	0.266351	0.0868854	0	0
0.0237171	0.064633	71726.6	RowBox[{-, 1217.39}]	RowBox[{-, 8.21431}]	0.287895	0.0903793	0	0
0.0237171	0.0861774	107788.	RowBox[{-, 391.773}]	RowBox[{-, 25.525}]	0.330984	0.0968973	0	0
0.0237171	0.0969496	128798.	RowBox[{-, 265.177}]	RowBox[{-, 37.7106}]	0.352528	0.099974	0	0
0.0237171	0.107722	151760.	RowBox[{-, 190.311}]	RowBox[{-, 52.5456}]	0.374072	0.102951	0	0
0.0237171	0.118494	176661.	RowBox[{-, 142.345}]	RowBox[{-, 70.2519}]	0.395617	0.105838	0	0
0.0237171	0.129266	203492.	RowBox[{-, 109.828}]	RowBox[{-, 91.0513}]	0.417161	0.108645	0	0
0.0237171	0.161583	295522.	RowBox[{-, 57.3965}]	RowBox[{-, 174.227}]	0.481794	0.116648	0	0
0.0237171	0.215443	487231.	RowBox[{-, 25.2894}]	RowBox[{-, 395.423}]	0.589516	0.128866	0	0
0.0252982	0.00215443	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	2881.	3.47101	0.1661	RowBox[{RowBox[{0.0486673, }], +, RowBox[{0.0486673, , i}]}]	0	0
0.0252982	0.0107722	33313.	2364.46	4.2293	0.183335	0.0663826	0	0
0.0252982	0.0161583	27934.7	2259.24	4.42626	0.194108	0.0711255	0	0
0.0252982	0.0215443	27997.9	2284.73	4.37688	0.20488	0.0742669	0	0
0.0252982	0.0538609	56789.9	RowBox[{-, 3779.93}]	RowBox[{-, 2.64555}]	0.269513	0.0868854	0	0
0.0252982	0.064633	71726.6	RowBox[{-, 1217.39}]	RowBox[{-, 8.21431}]	0.291057	0.0903793	0	0
0.0252982	0.0861774	107788.	RowBox[{-, 391.773}]	RowBox[{-, 25.525}]	0.334146	0.0968973	0	0
0.0252982	0.0969496	128798.	RowBox[{-, 265.177}]	RowBox[{-, 37.7106}]	0.35569	0.099974	0	0
0.0252982	0.107722	151760.	RowBox[{-, 190.311}]	RowBox[{-, 52.5456}]	0.377235	0.102951	0	0
0.0252982	0.118494	176661.	RowBox[{-, 142.345}]	RowBox[{-, 70.2519}]	0.398779	0.105838	0	0
0.0252982	0.129266	203492.	RowBox[{-, 109.828}]	RowBox[{-, 91.0513}]	0.420323	0.108645	0	0
0.0252982	0.161583	295522.	RowBox[{-, 57.3965}]	RowBox[{-, 174.227}]	0.484956	0.116648	0	0
0.0252982	0.215443	487231.	RowBox[{-, 25.2894}]	RowBox[{-, 395.423}]	0.592678	0.128866	0	0
0.0268794	0.00215443	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	2881.	3.47101	0.169262	RowBox[{RowBox[{0.0486673, }], +, RowBox[{0.0486673, , i}]}]	0	0
0.0268794	0.0107722	33313.	2364.46	4.2293	0.186498	0.0663826	0	0
0.0268794	0.0161583	27934.7	2259.24	4.42626	0.19727	0.0711255	0	0
0.0268794	0.0215443	27997.9	2284.73	4.37688	0.208042	0.0742669	0	0
0.0268794	0.0538609	56789.9	RowBox[{-, 3779.93}]	RowBox[{-, 2.64555}]	0.272675	0.0868854	0	0
0.0268794	0.064633	71726.6	RowBox[{-, 1217.39}]	RowBox[{-, 8.21431}]	0.294219	0.0903793	0	0
0.0268794	0.0861774	107788.	RowBox[{-, 391.773}]	RowBox[{-, 25.525}]	0.337308	0.0968973	0	0
0.0268794	0.0969496	128798.	RowBox[{-, 265.177}]	RowBox[{-, 37.7106}]	0.358853	0.099974	0	0
0.0268794	0.107722	151760.	RowBox[{-, 190.311}]	RowBox[{-, 52.5456}]	0.380397	0.102951	0	0
0.0268794	0.118494	176661.	RowBox[{-, 142.345}]	RowBox[{-, 70.2519}]	0.401941	0.105838	0	0
0.0268794	0.129266	203492.	RowBox[{-, 109.828}]	RowBox[{-, 91.0513}]	0.423486	0.108645	0	0
0.0268794	0.161583	295522.	RowBox[{-, 57.3965}]	RowBox[{-, 174.227}]	0.488119	0.116648	0	0
0.0268794	0.215443	487231.	RowBox[{-, 25.2894}]	RowBox[{-, 395.423}]	0.59584	0.128866	0	0
0.0284605	0.00215443	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	2881.	3.47101	0.172425	RowBox[{RowBox[{0.0486673, }], +, RowBox[{0.0486673, , i}]}]	0	0
0.0284605	0.0107722	33313.	2364.46	4.2293	0.18966	0.0663826	0	0
0.0284605	0.0161583	27934.7	2259.24	4.42626	0.200432	0.0711255	0	0
0.0284605	0.0215443	27997.9	2284.73	4.37688	0.211204	0.0742669	0	0
0.0284605	0.0538609	56789.9	RowBox[{-, 3779.93}]	RowBox[{-, 2.64555}]	0.275837	0.0868854	0	0
0.0284605	0.064633	71726.6	RowBox[{-, 1217.39}]	RowBox[{-, 8.21431}]	0.297382	0.0903793	0	0
0.0284605	0.0861774	107788.	RowBox[{-, 391.773}]	RowBox[{-, 25.525}]	0.34047	0.0968973	0	0
0.0284605	0.0969496	128798.	RowBox[{-, 265.177}]	RowBox[{-, 37.7106}]	0.362015	0.099974	0	0
0.0284605	0.107722	151760.	RowBox[{-, 190.311}]	RowBox[{-, 52.5456}]	0.383559	0.102951	0	0
0.0284605	0.118494	176661.	RowBox[{-, 142.345}]	RowBox[{-, 70.2519}]	0.405104	0.105838	0	0
0.0284605	0.129266	203492.	RowBox[{-, 109.828}]	RowBox[{-, 91.0513}]	0.426648	0.108645	0	0
0.0284605	0.161583	295522.	RowBox[{-, 57.3965}]	RowBox[{-, 174.227}]	0.491281	0.116648	0	0
0.0284605	0.215443	487231.	RowBox[{-, 25.2894}]	RowBox[{-, 395.423}]	0.599003	0.128866	0	0
0.0316228	0.00215443	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	2881.	3.47101	0.178749	RowBox[{RowBox[{0.0486673, }], +, RowBox[{0.0486673, , i}]}]	0	0
0.0316228	0.0107722	33313.	2364.46	4.2293	0.195985	0.0663826	0	0
0.0316228	0.0161583	27934.7	2259.24	4.42626	0.206757	0.0711255	0	0
0.0316228	0.0215443	27997.9	2284.73	4.37688	0.217529	0.0742669	0	0
0.0316228	0.0538609	56789.9	RowBox[{-, 3779.93}]	RowBox[{-, 2.64555}]	0.282162	0.0868854	0	0
0.0316228	0.064633	71726.6	RowBox[{-, 1217.39}]	RowBox[{-, 8.21431}]	0.303706	0.0903793	0	0
0.0316228	0.0861774	107788.	RowBox[{-, 391.773}]	RowBox[{-, 25.525}]	0.346795	0.0968973	0	0
0.0316228	0.0969496	128798.	RowBox[{-, 265.177}]	RowBox[{-, 37.7106}]	0.368339	0.099974	0	0
0.0316228	0.107722	151760.	RowBox[{-, 190.311}]	RowBox[{-, 52.5456}]	0.389884	0.102951	0	0
0.0316228	0.118494	176661.	RowBox[{-, 142.345}]	RowBox[{-, 70.2519}]	0.411428	0.105838	0	0
0.0316228	0.129266	203492.	RowBox[{-, 109.828}]	RowBox[{-, 91.0513}]	0.432972	0.108645	0	0
0.0316228	0.161583	295522.	RowBox[{-, 57.3965}]	RowBox[{-, 174.227}]	0.497605	0.116648	0	0
0.0316228	0.215443	487231.	RowBox[{-, 25.2894}]	RowBox[{-, 395.423}]	0.605327	0.128866	0	0

$RowBox[{stainlesssteel420, , thrust = , , 50000, , vol in^3 = , , 164.733}]$

rBot	Wall	stress lbf	sp thrust	weight	dia	r max stress	min # noz	max # noz
0.0353553	0.00368403	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	RowBox[{-, 2197.44}]	RowBox[{-, 22.7537}]	0.268219	RowBox[{RowBox[{0.0832198, }], +, RowBox[{0.0832198, , i}]}]	0	0
0.0353553	0.0184202	33313.	RowBox[{-, 1804.33}]	RowBox[{-, 27.7111}]	0.297691	0.113513	0	0
0.0353553	0.0276302	27934.7	RowBox[{-, 1532.78}]	RowBox[{-, 32.6204}]	0.316111	0.121623	0	0
0.0353553	0.0368403	27997.9	RowBox[{-, 1279.13}]	RowBox[{-, 39.0891}]	0.334532	0.126995	0	0
0.0353553	0.0921008	56789.9	RowBox[{-, 422.245}]	RowBox[{-, 118.415}]	0.445053	0.148572	0	0
0.0353553	0.110521	71726.6	RowBox[{-, 305.589}]	RowBox[{-, 163.618}]	0.481893	0.154546	0	0
0.0353553	0.147361	107788.	RowBox[{-, 173.116}]	RowBox[{-, 288.824}]	0.555573	0.165692	0	0
0.0353553	0.165781	128798.	RowBox[{-, 134.754}]	RowBox[{-, 371.045}]	0.592414	0.170953	0	0
0.0353553	0.184202	151760.	RowBox[{-, 106.878}]	RowBox[{-, 467.824}]	0.629254	0.176043	0	0
0.0353553	0.202622	176661.	RowBox[{-, 86.1667}]	RowBox[{-, 580.27}]	0.666094	0.180981	0	0
0.0353553	0.221042	203492.	RowBox[{-, 70.4729}]	RowBox[{-, 709.493}]	0.702935	0.18578	0	0
0.0353553	0.276302	295522.	RowBox[{-, 41.3595}]	RowBox[{-, 1208.91}]	0.813456	0.199465	0	0
0.0353553	0.368403	487231.	RowBox[{-, 20.1584}]	RowBox[{-, 2480.35}]	0.997657	0.220359	0	0
0.0424264	0.00368403	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	RowBox[{-, 2197.44}]	RowBox[{-, 22.7537}]	0.282361	RowBox[{RowBox[{0.0832198, }], +, RowBox[{0.0832198, , i}]}]	0	0
0.0424264	0.0184202	33313.	RowBox[{-, 1804.33}]	RowBox[{-, 27.7111}]	0.311833	0.113513	0	0
0.0424264	0.0276302	27934.7	RowBox[{-, 1532.78}]	RowBox[{-, 32.6204}]	0.330254	0.121623	0	0
0.0424264	0.0368403	27997.9	RowBox[{-, 1279.13}]	RowBox[{-, 39.0891}]	0.348674	0.126995	0	0
0.0424264	0.0921008	56789.9	RowBox[{-, 422.245}]	RowBox[{-, 118.415}]	0.459195	0.148572	0	0
0.0424264	0.110521	71726.6	RowBox[{-, 305.589}]	RowBox[{-, 163.618}]	0.496035	0.154546	0	0
0.0424264	0.147361	107788.	RowBox[{-, 173.116}]	RowBox[{-, 288.824}]	0.569716	0.165692	0	0
0.0424264	0.165781	128798.	RowBox[{-, 134.754}]	RowBox[{-, 371.045}]	0.606556	0.170953	0	0
0.0424264	0.184202	151760.	RowBox[{-, 106.878}]	RowBox[{-, 467.824}]	0.643396	0.176043	0	0
0.0424264	0.202622	176661.	RowBox[{-, 86.1667}]	RowBox[{-, 580.27}]	0.680237	0.180981	0	0
0.0424264	0.221042	203492.	RowBox[{-, 70.4729}]	RowBox[{-, 709.493}]	0.717077	0.18578	0	0
0.0424264	0.276302	295522.	RowBox[{-, 41.3595}]	RowBox[{-, 1208.91}]	0.827598	0.199465	0	0
0.0424264	0.368403	487231.	RowBox[{-, 20.1584}]	RowBox[{-, 2480.35}]	1.0118	0.220359	0	0
0.0459619	0.00368403	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	RowBox[{-, 2197.44}]	RowBox[{-, 22.7537}]	0.289432	RowBox[{RowBox[{0.0832198, }], +, RowBox[{0.0832198, , i}]}]	0	0
0.0459619	0.0184202	33313.	RowBox[{-, 1804.33}]	RowBox[{-, 27.7111}]	0.318904	0.113513	0	0
0.0459619	0.0276302	27934.7	RowBox[{-, 1532.78}]	RowBox[{-, 32.6204}]	0.337325	0.121623	0	0
0.0459619	0.0368403	27997.9	RowBox[{-, 1279.13}]	RowBox[{-, 39.0891}]	0.355745	0.126995	0	0
0.0459619	0.0921008	56789.9	RowBox[{-, 422.245}]	RowBox[{-, 118.415}]	0.466266	0.148572	0	0
0.0459619	0.110521	71726.6	RowBox[{-, 305.589}]	RowBox[{-, 163.618}]	0.503106	0.154546	0	0
0.0459619	0.147361	107788.	RowBox[{-, 173.116}]	RowBox[{-, 288.824}]	0.576787	0.165692	0	0
0.0459619	0.165781	128798.	RowBox[{-, 134.754}]	RowBox[{-, 371.045}]	0.613627	0.170953	0	0
0.0459619	0.184202	151760.	RowBox[{-, 106.878}]	RowBox[{-, 467.824}]	0.650467	0.176043	0	0
0.0459619	0.202622	176661.	RowBox[{-, 86.1667}]	RowBox[{-, 580.27}]	0.687308	0.180981	0	0
0.0459619	0.221042	203492.	RowBox[{-, 70.4729}]	RowBox[{-, 709.493}]	0.724148	0.18578	0	0
0.0459619	0.276302	295522.	RowBox[{-, 41.3595}]	RowBox[{-, 1208.91}]	0.834669	0.199465	0	0
0.0459619	0.368403	487231.	RowBox[{-, 20.1584}]	RowBox[{-, 2480.35}]	1.01887	0.220359	0	0
0.0494975	0.00368403	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	RowBox[{-, 2197.44}]	RowBox[{-, 22.7537}]	0.296503	RowBox[{RowBox[{0.0832198, }], +, RowBox[{0.0832198, , i}]}]	0	0
0.0494975	0.0184202	33313.	RowBox[{-, 1804.33}]	RowBox[{-, 27.7111}]	0.325976	0.113513	0	0
0.0494975	0.0276302	27934.7	RowBox[{-, 1532.78}]	RowBox[{-, 32.6204}]	0.344396	0.121623	0	0
0.0494975	0.0368403	27997.9	RowBox[{-, 1279.13}]	RowBox[{-, 39.0891}]	0.362816	0.126995	0	0
0.0494975	0.0921008	56789.9	RowBox[{-, 422.245}]	RowBox[{-, 118.415}]	0.473337	0.148572	0	0
0.0494975	0.110521	71726.6	RowBox[{-, 305.589}]	RowBox[{-, 163.618}]	0.510177	0.154546	0	0
0.0494975	0.147361	107788.	RowBox[{-, 173.116}]	RowBox[{-, 288.824}]	0.583858	0.165692	0	0
0.0494975	0.165781	128798.	RowBox[{-, 134.754}]	RowBox[{-, 371.045}]	0.620698	0.170953	0	0
0.0494975	0.184202	151760.	RowBox[{-, 106.878}]	RowBox[{-, 467.824}]	0.657538	0.176043	0	0
0.0494975	0.202622	176661.	RowBox[{-, 86.1667}]	RowBox[{-, 580.27}]	0.694379	0.180981	0	0
0.0494975	0.221042	203492.	RowBox[{-, 70.4729}]	RowBox[{-, 709.493}]	0.731219	0.18578	0	0
0.0494975	0.276302	295522.	RowBox[{-, 41.3595}]	RowBox[{-, 1208.91}]	0.84174	0.199465	0	0
0.0494975	0.368403	487231.	RowBox[{-, 20.1584}]	RowBox[{-, 2480.35}]	1.02594	0.220359	0	0
0.053033	0.00368403	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	RowBox[{-, 2197.44}]	RowBox[{-, 22.7537}]	0.303574	RowBox[{RowBox[{0.0832198, }], +, RowBox[{0.0832198, , i}]}]	0	0
0.053033	0.0184202	33313.	RowBox[{-, 1804.33}]	RowBox[{-, 27.7111}]	0.333047	0.113513	0	0
0.053033	0.0276302	27934.7	RowBox[{-, 1532.78}]	RowBox[{-, 32.6204}]	0.351467	0.121623	0	0
0.053033	0.0368403	27997.9	RowBox[{-, 1279.13}]	RowBox[{-, 39.0891}]	0.369887	0.126995	0	0
0.053033	0.0921008	56789.9	RowBox[{-, 422.245}]	RowBox[{-, 118.415}]	0.480408	0.148572	0	0
0.053033	0.110521	71726.6	RowBox[{-, 305.589}]	RowBox[{-, 163.618}]	0.517248	0.154546	0	0
0.053033	0.147361	107788.	RowBox[{-, 173.116}]	RowBox[{-, 288.824}]	0.590929	0.165692	0	0
0.053033	0.165781	128798.	RowBox[{-, 134.754}]	RowBox[{-, 371.045}]	0.627769	0.170953	0	0
0.053033	0.184202	151760.	RowBox[{-, 106.878}]	RowBox[{-, 467.824}]	0.664609	0.176043	0	0
0.053033	0.202622	176661.	RowBox[{-, 86.1667}]	RowBox[{-, 580.27}]	0.70145	0.180981	0	0
0.053033	0.221042	203492.	RowBox[{-, 70.4729}]	RowBox[{-, 709.493}]	0.73829	0.18578	0	0
0.053033	0.276302	295522.	RowBox[{-, 41.3595}]	RowBox[{-, 1208.91}]	0.848811	0.199465	0	0
0.053033	0.368403	487231.	RowBox[{-, 20.1584}]	RowBox[{-, 2480.35}]	1.03301	0.220359	0	0
0.0565685	0.00368403	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	RowBox[{-, 2197.44}]	RowBox[{-, 22.7537}]	0.310645	RowBox[{RowBox[{0.0832198, }], +, RowBox[{0.0832198, , i}]}]	0	0
0.0565685	0.0184202	33313.	RowBox[{-, 1804.33}]	RowBox[{-, 27.7111}]	0.340118	0.113513	0	0
0.0565685	0.0276302	27934.7	RowBox[{-, 1532.78}]	RowBox[{-, 32.6204}]	0.358538	0.121623	0	0
0.0565685	0.0368403	27997.9	RowBox[{-, 1279.13}]	RowBox[{-, 39.0891}]	0.376958	0.126995	0	0
0.0565685	0.0921008	56789.9	RowBox[{-, 422.245}]	RowBox[{-, 118.415}]	0.487479	0.148572	0	0
0.0565685	0.110521	71726.6	RowBox[{-, 305.589}]	RowBox[{-, 163.618}]	0.524319	0.154546	0	0
0.0565685	0.147361	107788.	RowBox[{-, 173.116}]	RowBox[{-, 288.824}]	0.598	0.165692	0	0
0.0565685	0.165781	128798.	RowBox[{-, 134.754}]	RowBox[{-, 371.045}]	0.63484	0.170953	0	0
0.0565685	0.184202	151760.	RowBox[{-, 106.878}]	RowBox[{-, 467.824}]	0.67168	0.176043	0	0
0.0565685	0.202622	176661.	RowBox[{-, 86.1667}]	RowBox[{-, 580.27}]	0.708521	0.180981	0	0
0.0565685	0.221042	203492.	RowBox[{-, 70.4729}]	RowBox[{-, 709.493}]	0.745361	0.18578	0	0
0.0565685	0.276302	295522.	RowBox[{-, 41.3595}]	RowBox[{-, 1208.91}]	0.855882	0.199465	0	0
0.0565685	0.368403	487231.	RowBox[{-, 20.1584}]	RowBox[{-, 2480.35}]	1.04008	0.220359	0	0
0.0601041	0.00368403	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	RowBox[{-, 2197.44}]	RowBox[{-, 22.7537}]	0.317716	RowBox[{RowBox[{0.0832198, }], +, RowBox[{0.0832198, , i}]}]	0	0
0.0601041	0.0184202	33313.	RowBox[{-, 1804.33}]	RowBox[{-, 27.7111}]	0.347189	0.113513	0	0
0.0601041	0.0276302	27934.7	RowBox[{-, 1532.78}]	RowBox[{-, 32.6204}]	0.365609	0.121623	0	0
0.0601041	0.0368403	27997.9	RowBox[{-, 1279.13}]	RowBox[{-, 39.0891}]	0.384029	0.126995	0	0
0.0601041	0.0921008	56789.9	RowBox[{-, 422.245}]	RowBox[{-, 118.415}]	0.49455	0.148572	0	0
0.0601041	0.110521	71726.6	RowBox[{-, 305.589}]	RowBox[{-, 163.618}]	0.53139	0.154546	0	0
0.0601041	0.147361	107788.	RowBox[{-, 173.116}]	RowBox[{-, 288.824}]	0.605071	0.165692	0	0
0.0601041	0.165781	128798.	RowBox[{-, 134.754}]	RowBox[{-, 371.045}]	0.641911	0.170953	0	0
0.0601041	0.184202	151760.	RowBox[{-, 106.878}]	RowBox[{-, 467.824}]	0.678752	0.176043	0	0
0.0601041	0.202622	176661.	RowBox[{-, 86.1667}]	RowBox[{-, 580.27}]	0.715592	0.180981	0	0
0.0601041	0.221042	203492.	RowBox[{-, 70.4729}]	RowBox[{-, 709.493}]	0.752432	0.18578	0	0
0.0601041	0.276302	295522.	RowBox[{-, 41.3595}]	RowBox[{-, 1208.91}]	0.862953	0.199465	0	0
0.0601041	0.368403	487231.	RowBox[{-, 20.1584}]	RowBox[{-, 2480.35}]	1.04715	0.220359	0	0
0.0636396	0.00368403	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	RowBox[{-, 2197.44}]	RowBox[{-, 22.7537}]	0.324788	RowBox[{RowBox[{0.0832198, }], +, RowBox[{0.0832198, , i}]}]	0	0
0.0636396	0.0184202	33313.	RowBox[{-, 1804.33}]	RowBox[{-, 27.7111}]	0.35426	0.113513	0	0
0.0636396	0.0276302	27934.7	RowBox[{-, 1532.78}]	RowBox[{-, 32.6204}]	0.37268	0.121623	0	0
0.0636396	0.0368403	27997.9	RowBox[{-, 1279.13}]	RowBox[{-, 39.0891}]	0.3911	0.126995	0	0
0.0636396	0.0921008	56789.9	RowBox[{-, 422.245}]	RowBox[{-, 118.415}]	0.501621	0.148572	0	0
0.0636396	0.110521	71726.6	RowBox[{-, 305.589}]	RowBox[{-, 163.618}]	0.538461	0.154546	0	0
0.0636396	0.147361	107788.	RowBox[{-, 173.116}]	RowBox[{-, 288.824}]	0.612142	0.165692	0	0
0.0636396	0.165781	128798.	RowBox[{-, 134.754}]	RowBox[{-, 371.045}]	0.648982	0.170953	0	0
0.0636396	0.184202	151760.	RowBox[{-, 106.878}]	RowBox[{-, 467.824}]	0.685823	0.176043	0	0
0.0636396	0.202622	176661.	RowBox[{-, 86.1667}]	RowBox[{-, 580.27}]	0.722663	0.180981	0	0
0.0636396	0.221042	203492.	RowBox[{-, 70.4729}]	RowBox[{-, 709.493}]	0.759503	0.18578	0	0
0.0636396	0.276302	295522.	RowBox[{-, 41.3595}]	RowBox[{-, 1208.91}]	0.870024	0.199465	0	0
0.0636396	0.368403	487231.	RowBox[{-, 20.1584}]	RowBox[{-, 2480.35}]	1.05423	0.220359	0	0
0.0707107	0.00368403	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	RowBox[{-, 2197.44}]	RowBox[{-, 22.7537}]	0.33893	RowBox[{RowBox[{0.0832198, }], +, RowBox[{0.0832198, , i}]}]	0	0
0.0707107	0.0184202	33313.	RowBox[{-, 1804.33}]	RowBox[{-, 27.7111}]	0.368402	0.113513	0	0
0.0707107	0.0276302	27934.7	RowBox[{-, 1532.78}]	RowBox[{-, 32.6204}]	0.386822	0.121623	0	0
0.0707107	0.0368403	27997.9	RowBox[{-, 1279.13}]	RowBox[{-, 39.0891}]	0.405242	0.126995	0	0
0.0707107	0.0921008	56789.9	RowBox[{-, 422.245}]	RowBox[{-, 118.415}]	0.515763	0.148572	0	0
0.0707107	0.110521	71726.6	RowBox[{-, 305.589}]	RowBox[{-, 163.618}]	0.552604	0.154546	0	0
0.0707107	0.147361	107788.	RowBox[{-, 173.116}]	RowBox[{-, 288.824}]	0.626284	0.165692	0	0
0.0707107	0.165781	128798.	RowBox[{-, 134.754}]	RowBox[{-, 371.045}]	0.663124	0.170953	0	0
0.0707107	0.184202	151760.	RowBox[{-, 106.878}]	RowBox[{-, 467.824}]	0.699965	0.176043	0	0
0.0707107	0.202622	176661.	RowBox[{-, 86.1667}]	RowBox[{-, 580.27}]	0.736805	0.180981	0	0
0.0707107	0.221042	203492.	RowBox[{-, 70.4729}]	RowBox[{-, 709.493}]	0.773645	0.18578	0	0
0.0707107	0.276302	295522.	RowBox[{-, 41.3595}]	RowBox[{-, 1208.91}]	0.884166	0.199465	0	0
0.0707107	0.368403	487231.	RowBox[{-, 20.1584}]	RowBox[{-, 2480.35}]	1.06837	0.220359	0	0

$RowBox[{stainlesssteel420, , thrust = , , 100000, , vol in^3 = , , 329.466}]$

rBot	Wall	stress lbf	sp thrust	weight	dia	r max stress	min # noz	max # noz
0.05	0.00464159	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	RowBox[{-, 1448.04}]	RowBox[{-, 69.0591}]	0.348845	RowBox[{RowBox[{0.10485, }], +, RowBox[{0.10485, , i}]}]	0	0
0.05	0.0232079	33313.	RowBox[{-, 1189.65}]	RowBox[{-, 84.0581}]	0.385978	0.143017	0	0
0.05	0.0348119	27934.7	RowBox[{-, 1027.73}]	RowBox[{-, 97.302}]	0.409186	0.153235	0	0
0.05	0.0464159	27997.9	RowBox[{-, 878.309}]	RowBox[{-, 113.855}]	0.432393	0.160003	0	0
0.05	0.11604	56789.9	RowBox[{-, 335.344}]	RowBox[{-, 298.201}]	0.571641	0.187189	0	0
0.05	0.139248	71726.6	RowBox[{-, 250.817}]	RowBox[{-, 398.697}]	0.618057	0.194716	0	0
0.05	0.185664	107788.	RowBox[{-, 148.904}]	RowBox[{-, 671.572}]	0.710889	0.208759	0	0
0.05	0.208871	128798.	RowBox[{-, 117.871}]	RowBox[{-, 848.388}]	0.757305	0.215388	0	0
0.05	0.232079	151760.	RowBox[{-, 94.7794}]	RowBox[{-, 1055.08}]	0.803721	0.221801	0	0
0.05	0.255287	176661.	RowBox[{-, 77.2874}]	RowBox[{-, 1293.87}]	0.850136	0.228021	0	0
0.05	0.278495	203492.	RowBox[{-, 63.8172}]	RowBox[{-, 1566.98}]	0.896552	0.234069	0	0
0.05	0.348119	295522.	RowBox[{-, 38.2502}]	RowBox[{-, 2614.37}]	1.0358	0.25131	0	0
0.05	0.464159	487231.	RowBox[{-, 19.0353}]	RowBox[{-, 5253.4}]	1.26788	0.277634	0	0
0.06	0.00464159	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	RowBox[{-, 1448.04}]	RowBox[{-, 69.0591}]	0.368845	RowBox[{RowBox[{0.10485, }], +, RowBox[{0.10485, , i}]}]	0	0
0.06	0.0232079	33313.	RowBox[{-, 1189.65}]	RowBox[{-, 84.0581}]	0.405978	0.143017	0	0
0.06	0.0348119	27934.7	RowBox[{-, 1027.73}]	RowBox[{-, 97.302}]	0.429186	0.153235	0	0
0.06	0.0464159	27997.9	RowBox[{-, 878.309}]	RowBox[{-, 113.855}]	0.452393	0.160003	0	0
0.06	0.11604	56789.9	RowBox[{-, 335.344}]	RowBox[{-, 298.201}]	0.591641	0.187189	0	0
0.06	0.139248	71726.6	RowBox[{-, 250.817}]	RowBox[{-, 398.697}]	0.638057	0.194716	0	0
0.06	0.185664	107788.	RowBox[{-, 148.904}]	RowBox[{-, 671.572}]	0.730889	0.208759	0	0
0.06	0.208871	128798.	RowBox[{-, 117.871}]	RowBox[{-, 848.388}]	0.777305	0.215388	0	0
0.06	0.232079	151760.	RowBox[{-, 94.7794}]	RowBox[{-, 1055.08}]	0.823721	0.221801	0	0
0.06	0.255287	176661.	RowBox[{-, 77.2874}]	RowBox[{-, 1293.87}]	0.870136	0.228021	0	0
0.06	0.278495	203492.	RowBox[{-, 63.8172}]	RowBox[{-, 1566.98}]	0.916552	0.234069	0	0
0.06	0.348119	295522.	RowBox[{-, 38.2502}]	RowBox[{-, 2614.37}]	1.0558	0.25131	0	0
0.06	0.464159	487231.	RowBox[{-, 19.0353}]	RowBox[{-, 5253.4}]	1.28788	0.277634	0	0
0.065	0.00464159	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	RowBox[{-, 1448.04}]	RowBox[{-, 69.0591}]	0.378845	RowBox[{RowBox[{0.10485, }], +, RowBox[{0.10485, , i}]}]	0	0
0.065	0.0232079	33313.	RowBox[{-, 1189.65}]	RowBox[{-, 84.0581}]	0.415978	0.143017	0	0
0.065	0.0348119	27934.7	RowBox[{-, 1027.73}]	RowBox[{-, 97.302}]	0.439186	0.153235	0	0
0.065	0.0464159	27997.9	RowBox[{-, 878.309}]	RowBox[{-, 113.855}]	0.462393	0.160003	0	0
0.065	0.11604	56789.9	RowBox[{-, 335.344}]	RowBox[{-, 298.201}]	0.601641	0.187189	0	0
0.065	0.139248	71726.6	RowBox[{-, 250.817}]	RowBox[{-, 398.697}]	0.648057	0.194716	0	0
0.065	0.185664	107788.	RowBox[{-, 148.904}]	RowBox[{-, 671.572}]	0.740889	0.208759	0	0
0.065	0.208871	128798.	RowBox[{-, 117.871}]	RowBox[{-, 848.388}]	0.787305	0.215388	0	0
0.065	0.232079	151760.	RowBox[{-, 94.7794}]	RowBox[{-, 1055.08}]	0.833721	0.221801	0	0
0.065	0.255287	176661.	RowBox[{-, 77.2874}]	RowBox[{-, 1293.87}]	0.880136	0.228021	0	0
0.065	0.278495	203492.	RowBox[{-, 63.8172}]	RowBox[{-, 1566.98}]	0.926552	0.234069	0	0
0.065	0.348119	295522.	RowBox[{-, 38.2502}]	RowBox[{-, 2614.37}]	1.0658	0.25131	0	0
0.065	0.464159	487231.	RowBox[{-, 19.0353}]	RowBox[{-, 5253.4}]	1.29788	0.277634	0	0
0.07	0.00464159	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	RowBox[{-, 1448.04}]	RowBox[{-, 69.0591}]	0.388845	RowBox[{RowBox[{0.10485, }], +, RowBox[{0.10485, , i}]}]	0	0
0.07	0.0232079	33313.	RowBox[{-, 1189.65}]	RowBox[{-, 84.0581}]	0.425978	0.143017	0	0
0.07	0.0348119	27934.7	RowBox[{-, 1027.73}]	RowBox[{-, 97.302}]	0.449186	0.153235	0	0
0.07	0.0464159	27997.9	RowBox[{-, 878.309}]	RowBox[{-, 113.855}]	0.472393	0.160003	0	0
0.07	0.11604	56789.9	RowBox[{-, 335.344}]	RowBox[{-, 298.201}]	0.611641	0.187189	0	0
0.07	0.139248	71726.6	RowBox[{-, 250.817}]	RowBox[{-, 398.697}]	0.658057	0.194716	0	0
0.07	0.185664	107788.	RowBox[{-, 148.904}]	RowBox[{-, 671.572}]	0.750889	0.208759	0	0
0.07	0.208871	128798.	RowBox[{-, 117.871}]	RowBox[{-, 848.388}]	0.797305	0.215388	0	0
0.07	0.232079	151760.	RowBox[{-, 94.7794}]	RowBox[{-, 1055.08}]	0.843721	0.221801	0	0
0.07	0.255287	176661.	RowBox[{-, 77.2874}]	RowBox[{-, 1293.87}]	0.890136	0.228021	0	0
0.07	0.278495	203492.	RowBox[{-, 63.8172}]	RowBox[{-, 1566.98}]	0.936552	0.234069	0	0
0.07	0.348119	295522.	RowBox[{-, 38.2502}]	RowBox[{-, 2614.37}]	1.0758	0.25131	0	0
0.07	0.464159	487231.	RowBox[{-, 19.0353}]	RowBox[{-, 5253.4}]	1.30788	0.277634	0	0
0.075	0.00464159	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	RowBox[{-, 1448.04}]	RowBox[{-, 69.0591}]	0.398845	RowBox[{RowBox[{0.10485, }], +, RowBox[{0.10485, , i}]}]	0	0
0.075	0.0232079	33313.	RowBox[{-, 1189.65}]	RowBox[{-, 84.0581}]	0.435978	0.143017	0	0
0.075	0.0348119	27934.7	RowBox[{-, 1027.73}]	RowBox[{-, 97.302}]	0.459186	0.153235	0	0
0.075	0.0464159	27997.9	RowBox[{-, 878.309}]	RowBox[{-, 113.855}]	0.482393	0.160003	0	0
0.075	0.11604	56789.9	RowBox[{-, 335.344}]	RowBox[{-, 298.201}]	0.621641	0.187189	0	0
0.075	0.139248	71726.6	RowBox[{-, 250.817}]	RowBox[{-, 398.697}]	0.668057	0.194716	0	0
0.075	0.185664	107788.	RowBox[{-, 148.904}]	RowBox[{-, 671.572}]	0.760889	0.208759	0	0
0.075	0.208871	128798.	RowBox[{-, 117.871}]	RowBox[{-, 848.388}]	0.807305	0.215388	0	0
0.075	0.232079	151760.	RowBox[{-, 94.7794}]	RowBox[{-, 1055.08}]	0.853721	0.221801	0	0
0.075	0.255287	176661.	RowBox[{-, 77.2874}]	RowBox[{-, 1293.87}]	0.900136	0.228021	0	0
0.075	0.278495	203492.	RowBox[{-, 63.8172}]	RowBox[{-, 1566.98}]	0.946552	0.234069	0	0
0.075	0.348119	295522.	RowBox[{-, 38.2502}]	RowBox[{-, 2614.37}]	1.0858	0.25131	0	0
0.075	0.464159	487231.	RowBox[{-, 19.0353}]	RowBox[{-, 5253.4}]	1.31788	0.277634	0	0
0.08	0.00464159	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	RowBox[{-, 1448.04}]	RowBox[{-, 69.0591}]	0.408845	RowBox[{RowBox[{0.10485, }], +, RowBox[{0.10485, , i}]}]	0	0
0.08	0.0232079	33313.	RowBox[{-, 1189.65}]	RowBox[{-, 84.0581}]	0.445978	0.143017	0	0
0.08	0.0348119	27934.7	RowBox[{-, 1027.73}]	RowBox[{-, 97.302}]	0.469186	0.153235	0	0
0.08	0.0464159	27997.9	RowBox[{-, 878.309}]	RowBox[{-, 113.855}]	0.492393	0.160003	0	0
0.08	0.11604	56789.9	RowBox[{-, 335.344}]	RowBox[{-, 298.201}]	0.631641	0.187189	0	0
0.08	0.139248	71726.6	RowBox[{-, 250.817}]	RowBox[{-, 398.697}]	0.678057	0.194716	0	0
0.08	0.185664	107788.	RowBox[{-, 148.904}]	RowBox[{-, 671.572}]	0.770889	0.208759	0	0
0.08	0.208871	128798.	RowBox[{-, 117.871}]	RowBox[{-, 848.388}]	0.817305	0.215388	0	0
0.08	0.232079	151760.	RowBox[{-, 94.7794}]	RowBox[{-, 1055.08}]	0.863721	0.221801	0	0
0.08	0.255287	176661.	RowBox[{-, 77.2874}]	RowBox[{-, 1293.87}]	0.910136	0.228021	0	0
0.08	0.278495	203492.	RowBox[{-, 63.8172}]	RowBox[{-, 1566.98}]	0.956552	0.234069	0	0
0.08	0.348119	295522.	RowBox[{-, 38.2502}]	RowBox[{-, 2614.37}]	1.0958	0.25131	0	0
0.08	0.464159	487231.	RowBox[{-, 19.0353}]	RowBox[{-, 5253.4}]	1.32788	0.277634	0	0
0.085	0.00464159	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	RowBox[{-, 1448.04}]	RowBox[{-, 69.0591}]	0.418845	RowBox[{RowBox[{0.10485, }], +, RowBox[{0.10485, , i}]}]	0	0
0.085	0.0232079	33313.	RowBox[{-, 1189.65}]	RowBox[{-, 84.0581}]	0.455978	0.143017	0	0
0.085	0.0348119	27934.7	RowBox[{-, 1027.73}]	RowBox[{-, 97.302}]	0.479186	0.153235	0	0
0.085	0.0464159	27997.9	RowBox[{-, 878.309}]	RowBox[{-, 113.855}]	0.502393	0.160003	0	0
0.085	0.11604	56789.9	RowBox[{-, 335.344}]	RowBox[{-, 298.201}]	0.641641	0.187189	0	0
0.085	0.139248	71726.6	RowBox[{-, 250.817}]	RowBox[{-, 398.697}]	0.688057	0.194716	0	0
0.085	0.185664	107788.	RowBox[{-, 148.904}]	RowBox[{-, 671.572}]	0.780889	0.208759	0	0
0.085	0.208871	128798.	RowBox[{-, 117.871}]	RowBox[{-, 848.388}]	0.827305	0.215388	0	0
0.085	0.232079	151760.	RowBox[{-, 94.7794}]	RowBox[{-, 1055.08}]	0.873721	0.221801	0	0
0.085	0.255287	176661.	RowBox[{-, 77.2874}]	RowBox[{-, 1293.87}]	0.920136	0.228021	0	0
0.085	0.278495	203492.	RowBox[{-, 63.8172}]	RowBox[{-, 1566.98}]	0.966552	0.234069	0	0
0.085	0.348119	295522.	RowBox[{-, 38.2502}]	RowBox[{-, 2614.37}]	1.1058	0.25131	0	0
0.085	0.464159	487231.	RowBox[{-, 19.0353}]	RowBox[{-, 5253.4}]	1.33788	0.277634	0	0
0.09	0.00464159	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	RowBox[{-, 1448.04}]	RowBox[{-, 69.0591}]	0.428845	RowBox[{RowBox[{0.10485, }], +, RowBox[{0.10485, , i}]}]	0	0
0.09	0.0232079	33313.	RowBox[{-, 1189.65}]	RowBox[{-, 84.0581}]	0.465978	0.143017	0	0
0.09	0.0348119	27934.7	RowBox[{-, 1027.73}]	RowBox[{-, 97.302}]	0.489186	0.153235	0	0
0.09	0.0464159	27997.9	RowBox[{-, 878.309}]	RowBox[{-, 113.855}]	0.512393	0.160003	0	0
0.09	0.11604	56789.9	RowBox[{-, 335.344}]	RowBox[{-, 298.201}]	0.651641	0.187189	0	0
0.09	0.139248	71726.6	RowBox[{-, 250.817}]	RowBox[{-, 398.697}]	0.698057	0.194716	0	0
0.09	0.185664	107788.	RowBox[{-, 148.904}]	RowBox[{-, 671.572}]	0.790889	0.208759	0	0
0.09	0.208871	128798.	RowBox[{-, 117.871}]	RowBox[{-, 848.388}]	0.837305	0.215388	0	0
0.09	0.232079	151760.	RowBox[{-, 94.7794}]	RowBox[{-, 1055.08}]	0.883721	0.221801	0	0
0.09	0.255287	176661.	RowBox[{-, 77.2874}]	RowBox[{-, 1293.87}]	0.930136	0.228021	0	0
0.09	0.278495	203492.	RowBox[{-, 63.8172}]	RowBox[{-, 1566.98}]	0.976552	0.234069	0	0
0.09	0.348119	295522.	RowBox[{-, 38.2502}]	RowBox[{-, 2614.37}]	1.1158	0.25131	0	0
0.09	0.464159	487231.	RowBox[{-, 19.0353}]	RowBox[{-, 5253.4}]	1.34788	0.277634	0	0
0.1	0.00464159	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	RowBox[{-, 1448.04}]	RowBox[{-, 69.0591}]	0.448845	RowBox[{RowBox[{0.10485, }], +, RowBox[{0.10485, , i}]}]	0	0
0.1	0.0232079	33313.	RowBox[{-, 1189.65}]	RowBox[{-, 84.0581}]	0.485978	0.143017	0	0
0.1	0.0348119	27934.7	RowBox[{-, 1027.73}]	RowBox[{-, 97.302}]	0.509186	0.153235	0	0
0.1	0.0464159	27997.9	RowBox[{-, 878.309}]	RowBox[{-, 113.855}]	0.532393	0.160003	0	0
0.1	0.11604	56789.9	RowBox[{-, 335.344}]	RowBox[{-, 298.201}]	0.671641	0.187189	0	0
0.1	0.139248	71726.6	RowBox[{-, 250.817}]	RowBox[{-, 398.697}]	0.718057	0.194716	0	0
0.1	0.185664	107788.	RowBox[{-, 148.904}]	RowBox[{-, 671.572}]	0.810889	0.208759	0	0
0.1	0.208871	128798.	RowBox[{-, 117.871}]	RowBox[{-, 848.388}]	0.857305	0.215388	0	0
0.1	0.232079	151760.	RowBox[{-, 94.7794}]	RowBox[{-, 1055.08}]	0.903721	0.221801	0	0
0.1	0.255287	176661.	RowBox[{-, 77.2874}]	RowBox[{-, 1293.87}]	0.950136	0.228021	0	0
0.1	0.278495	203492.	RowBox[{-, 63.8172}]	RowBox[{-, 1566.98}]	0.996552	0.234069	0	0
0.1	0.348119	295522.	RowBox[{-, 38.2502}]	RowBox[{-, 2614.37}]	1.1358	0.25131	0	0
0.1	0.464159	487231.	RowBox[{-, 19.0353}]	RowBox[{-, 5253.4}]	1.36788	0.277634	0	0

$RowBox[{stainlesssteel420, , thrust = , , 500000, , vol in^3 = , , 1647.33}]$

rBot	Wall	stress lbf	sp thrust	weight	dia	r max stress	min # noz	max # noz
0.111803	0.00793701	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	RowBox[{-, 935.393}]	RowBox[{-, 534.535}]	0.649126	RowBox[{RowBox[{0.179292, }], +, RowBox[{0.179292, , i}]}]	0	0
0.111803	0.039685	33313.	RowBox[{-, 769.067}]	RowBox[{-, 650.138}]	0.712622	0.244556	0	0
0.111803	0.0595275	27934.7	RowBox[{-, 672.3}]	RowBox[{-, 743.715}]	0.752307	0.262029	0	0
0.111803	0.0793701	27997.9	RowBox[{-, 584.549}]	RowBox[{-, 855.361}]	0.791992	0.273601	0	0
0.111803	0.198425	56789.9	RowBox[{-, 252.231}]	RowBox[{-, 1982.31}]	1.0301	0.320088	0	0
0.111803	0.23811	71726.6	RowBox[{-, 194.904}]	RowBox[{-, 2565.37}]	1.10947	0.33296	0	0
0.111803	0.31748	107788.	RowBox[{-, 121.68}]	RowBox[{-, 4109.15}]	1.26821	0.356973	0	0
0.111803	0.357165	128798.	RowBox[{-, 98.192}]	RowBox[{-, 5092.06}]	1.34758	0.368308	0	0
0.111803	0.39685	151760.	RowBox[{-, 80.251}]	RowBox[{-, 6230.45}]	1.42695	0.379274	0	0
0.111803	0.436535	176661.	RowBox[{-, 66.3535}]	RowBox[{-, 7535.4}]	1.50632	0.389911	0	0
0.111803	0.47622	203492.	RowBox[{-, 55.4446}]	RowBox[{-, 9018.02}]	1.58569	0.400252	0	0
0.111803	0.595275	295522.	RowBox[{-, 34.1466}]	RowBox[{-, 14642.7}]	1.8238	0.429734	0	0
0.111803	0.793701	487231.	RowBox[{-, 17.4789}]	RowBox[{-, 28605.9}]	2.22065	0.474748	0	0
0.134164	0.00793701	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	RowBox[{-, 935.393}]	RowBox[{-, 534.535}]	0.693847	RowBox[{RowBox[{0.179292, }], +, RowBox[{0.179292, , i}]}]	0	0
0.134164	0.039685	33313.	RowBox[{-, 769.067}]	RowBox[{-, 650.138}]	0.757343	0.244556	0	0
0.134164	0.0595275	27934.7	RowBox[{-, 672.3}]	RowBox[{-, 743.715}]	0.797028	0.262029	0	0
0.134164	0.0793701	27997.9	RowBox[{-, 584.549}]	RowBox[{-, 855.361}]	0.836713	0.273601	0	0
0.134164	0.198425	56789.9	RowBox[{-, 252.231}]	RowBox[{-, 1982.31}]	1.07482	0.320088	0	0
0.134164	0.23811	71726.6	RowBox[{-, 194.904}]	RowBox[{-, 2565.37}]	1.15419	0.33296	0	0
0.134164	0.31748	107788.	RowBox[{-, 121.68}]	RowBox[{-, 4109.15}]	1.31293	0.356973	0	0
0.134164	0.357165	128798.	RowBox[{-, 98.192}]	RowBox[{-, 5092.06}]	1.3923	0.368308	0	0
0.134164	0.39685	151760.	RowBox[{-, 80.251}]	RowBox[{-, 6230.45}]	1.47167	0.379274	0	0
0.134164	0.436535	176661.	RowBox[{-, 66.3535}]	RowBox[{-, 7535.4}]	1.55104	0.389911	0	0
0.134164	0.47622	203492.	RowBox[{-, 55.4446}]	RowBox[{-, 9018.02}]	1.63041	0.400252	0	0
0.134164	0.595275	295522.	RowBox[{-, 34.1466}]	RowBox[{-, 14642.7}]	1.86852	0.429734	0	0
0.134164	0.793701	487231.	RowBox[{-, 17.4789}]	RowBox[{-, 28605.9}]	2.26537	0.474748	0	0
0.145344	0.00793701	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	RowBox[{-, 935.393}]	RowBox[{-, 534.535}]	0.716208	RowBox[{RowBox[{0.179292, }], +, RowBox[{0.179292, , i}]}]	0	0
0.145344	0.039685	33313.	RowBox[{-, 769.067}]	RowBox[{-, 650.138}]	0.779704	0.244556	0	0
0.145344	0.0595275	27934.7	RowBox[{-, 672.3}]	RowBox[{-, 743.715}]	0.819389	0.262029	0	0
0.145344	0.0793701	27997.9	RowBox[{-, 584.549}]	RowBox[{-, 855.361}]	0.859074	0.273601	0	0
0.145344	0.198425	56789.9	RowBox[{-, 252.231}]	RowBox[{-, 1982.31}]	1.09718	0.320088	0	0
0.145344	0.23811	71726.6	RowBox[{-, 194.904}]	RowBox[{-, 2565.37}]	1.17655	0.33296	0	0
0.145344	0.31748	107788.	RowBox[{-, 121.68}]	RowBox[{-, 4109.15}]	1.33529	0.356973	0	0
0.145344	0.357165	128798.	RowBox[{-, 98.192}]	RowBox[{-, 5092.06}]	1.41466	0.368308	0	0
0.145344	0.39685	151760.	RowBox[{-, 80.251}]	RowBox[{-, 6230.45}]	1.49403	0.379274	0	0
0.145344	0.436535	176661.	RowBox[{-, 66.3535}]	RowBox[{-, 7535.4}]	1.5734	0.389911	0	0
0.145344	0.47622	203492.	RowBox[{-, 55.4446}]	RowBox[{-, 9018.02}]	1.65277	0.400252	0	0
0.145344	0.595275	295522.	RowBox[{-, 34.1466}]	RowBox[{-, 14642.7}]	1.89088	0.429734	0	0
0.145344	0.793701	487231.	RowBox[{-, 17.4789}]	RowBox[{-, 28605.9}]	2.28773	0.474748	0	0
0.156525	0.00793701	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	RowBox[{-, 935.393}]	RowBox[{-, 534.535}]	0.738568	RowBox[{RowBox[{0.179292, }], +, RowBox[{0.179292, , i}]}]	0	0
0.156525	0.039685	33313.	RowBox[{-, 769.067}]	RowBox[{-, 650.138}]	0.802064	0.244556	0	0
0.156525	0.0595275	27934.7	RowBox[{-, 672.3}]	RowBox[{-, 743.715}]	0.841749	0.262029	0	0
0.156525	0.0793701	27997.9	RowBox[{-, 584.549}]	RowBox[{-, 855.361}]	0.881434	0.273601	0	0
0.156525	0.198425	56789.9	RowBox[{-, 252.231}]	RowBox[{-, 1982.31}]	1.11954	0.320088	0	0
0.156525	0.23811	71726.6	RowBox[{-, 194.904}]	RowBox[{-, 2565.37}]	1.19891	0.33296	0	0
0.156525	0.31748	107788.	RowBox[{-, 121.68}]	RowBox[{-, 4109.15}]	1.35765	0.356973	0	0
0.156525	0.357165	128798.	RowBox[{-, 98.192}]	RowBox[{-, 5092.06}]	1.43702	0.368308	0	0
0.156525	0.39685	151760.	RowBox[{-, 80.251}]	RowBox[{-, 6230.45}]	1.51639	0.379274	0	0
0.156525	0.436535	176661.	RowBox[{-, 66.3535}]	RowBox[{-, 7535.4}]	1.59576	0.389911	0	0
0.156525	0.47622	203492.	RowBox[{-, 55.4446}]	RowBox[{-, 9018.02}]	1.67513	0.400252	0	0
0.156525	0.595275	295522.	RowBox[{-, 34.1466}]	RowBox[{-, 14642.7}]	1.91325	0.429734	0	0
0.156525	0.793701	487231.	RowBox[{-, 17.4789}]	RowBox[{-, 28605.9}]	2.3101	0.474748	0	0
0.167705	0.00793701	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	RowBox[{-, 935.393}]	RowBox[{-, 534.535}]	0.760929	RowBox[{RowBox[{0.179292, }], +, RowBox[{0.179292, , i}]}]	0	0
0.167705	0.039685	33313.	RowBox[{-, 769.067}]	RowBox[{-, 650.138}]	0.824425	0.244556	0	0
0.167705	0.0595275	27934.7	RowBox[{-, 672.3}]	RowBox[{-, 743.715}]	0.86411	0.262029	0	0
0.167705	0.0793701	27997.9	RowBox[{-, 584.549}]	RowBox[{-, 855.361}]	0.903795	0.273601	0	0
0.167705	0.198425	56789.9	RowBox[{-, 252.231}]	RowBox[{-, 1982.31}]	1.14191	0.320088	0	0
0.167705	0.23811	71726.6	RowBox[{-, 194.904}]	RowBox[{-, 2565.37}]	1.22128	0.33296	0	0
0.167705	0.31748	107788.	RowBox[{-, 121.68}]	RowBox[{-, 4109.15}]	1.38002	0.356973	0	0
0.167705	0.357165	128798.	RowBox[{-, 98.192}]	RowBox[{-, 5092.06}]	1.45939	0.368308	0	0
0.167705	0.39685	151760.	RowBox[{-, 80.251}]	RowBox[{-, 6230.45}]	1.53876	0.379274	0	0
0.167705	0.436535	176661.	RowBox[{-, 66.3535}]	RowBox[{-, 7535.4}]	1.61813	0.389911	0	0
0.167705	0.47622	203492.	RowBox[{-, 55.4446}]	RowBox[{-, 9018.02}]	1.6975	0.400252	0	0
0.167705	0.595275	295522.	RowBox[{-, 34.1466}]	RowBox[{-, 14642.7}]	1.93561	0.429734	0	0
0.167705	0.793701	487231.	RowBox[{-, 17.4789}]	RowBox[{-, 28605.9}]	2.33246	0.474748	0	0
0.178885	0.00793701	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	RowBox[{-, 935.393}]	RowBox[{-, 534.535}]	0.78329	RowBox[{RowBox[{0.179292, }], +, RowBox[{0.179292, , i}]}]	0	0
0.178885	0.039685	33313.	RowBox[{-, 769.067}]	RowBox[{-, 650.138}]	0.846786	0.244556	0	0
0.178885	0.0595275	27934.7	RowBox[{-, 672.3}]	RowBox[{-, 743.715}]	0.886471	0.262029	0	0
0.178885	0.0793701	27997.9	RowBox[{-, 584.549}]	RowBox[{-, 855.361}]	0.926156	0.273601	0	0
0.178885	0.198425	56789.9	RowBox[{-, 252.231}]	RowBox[{-, 1982.31}]	1.16427	0.320088	0	0
0.178885	0.23811	71726.6	RowBox[{-, 194.904}]	RowBox[{-, 2565.37}]	1.24364	0.33296	0	0
0.178885	0.31748	107788.	RowBox[{-, 121.68}]	RowBox[{-, 4109.15}]	1.40238	0.356973	0	0
0.178885	0.357165	128798.	RowBox[{-, 98.192}]	RowBox[{-, 5092.06}]	1.48175	0.368308	0	0
0.178885	0.39685	151760.	RowBox[{-, 80.251}]	RowBox[{-, 6230.45}]	1.56112	0.379274	0	0
0.178885	0.436535	176661.	RowBox[{-, 66.3535}]	RowBox[{-, 7535.4}]	1.64049	0.389911	0	0
0.178885	0.47622	203492.	RowBox[{-, 55.4446}]	RowBox[{-, 9018.02}]	1.71986	0.400252	0	0
0.178885	0.595275	295522.	RowBox[{-, 34.1466}]	RowBox[{-, 14642.7}]	1.95797	0.429734	0	0
0.178885	0.793701	487231.	RowBox[{-, 17.4789}]	RowBox[{-, 28605.9}]	2.35482	0.474748	0	0
0.190066	0.00793701	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	RowBox[{-, 935.393}]	RowBox[{-, 534.535}]	0.80565	RowBox[{RowBox[{0.179292, }], +, RowBox[{0.179292, , i}]}]	0	0
0.190066	0.039685	33313.	RowBox[{-, 769.067}]	RowBox[{-, 650.138}]	0.869146	0.244556	0	0
0.190066	0.0595275	27934.7	RowBox[{-, 672.3}]	RowBox[{-, 743.715}]	0.908831	0.262029	0	0
0.190066	0.0793701	27997.9	RowBox[{-, 584.549}]	RowBox[{-, 855.361}]	0.948516	0.273601	0	0
0.190066	0.198425	56789.9	RowBox[{-, 252.231}]	RowBox[{-, 1982.31}]	1.18663	0.320088	0	0
0.190066	0.23811	71726.6	RowBox[{-, 194.904}]	RowBox[{-, 2565.37}]	1.266	0.33296	0	0
0.190066	0.31748	107788.	RowBox[{-, 121.68}]	RowBox[{-, 4109.15}]	1.42474	0.356973	0	0
0.190066	0.357165	128798.	RowBox[{-, 98.192}]	RowBox[{-, 5092.06}]	1.50411	0.368308	0	0
0.190066	0.39685	151760.	RowBox[{-, 80.251}]	RowBox[{-, 6230.45}]	1.58348	0.379274	0	0
0.190066	0.436535	176661.	RowBox[{-, 66.3535}]	RowBox[{-, 7535.4}]	1.66285	0.389911	0	0
0.190066	0.47622	203492.	RowBox[{-, 55.4446}]	RowBox[{-, 9018.02}]	1.74222	0.400252	0	0
0.190066	0.595275	295522.	RowBox[{-, 34.1466}]	RowBox[{-, 14642.7}]	1.98033	0.429734	0	0
0.190066	0.793701	487231.	RowBox[{-, 17.4789}]	RowBox[{-, 28605.9}]	2.37718	0.474748	0	0
0.201246	0.00793701	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	RowBox[{-, 935.393}]	RowBox[{-, 534.535}]	0.828011	RowBox[{RowBox[{0.179292, }], +, RowBox[{0.179292, , i}]}]	0	0
0.201246	0.039685	33313.	RowBox[{-, 769.067}]	RowBox[{-, 650.138}]	0.891507	0.244556	0	0
0.201246	0.0595275	27934.7	RowBox[{-, 672.3}]	RowBox[{-, 743.715}]	0.931192	0.262029	0	0
0.201246	0.0793701	27997.9	RowBox[{-, 584.549}]	RowBox[{-, 855.361}]	0.970877	0.273601	0	0
0.201246	0.198425	56789.9	RowBox[{-, 252.231}]	RowBox[{-, 1982.31}]	1.20899	0.320088	0	0
0.201246	0.23811	71726.6	RowBox[{-, 194.904}]	RowBox[{-, 2565.37}]	1.28836	0.33296	0	0
0.201246	0.31748	107788.	RowBox[{-, 121.68}]	RowBox[{-, 4109.15}]	1.4471	0.356973	0	0
0.201246	0.357165	128798.	RowBox[{-, 98.192}]	RowBox[{-, 5092.06}]	1.52647	0.368308	0	0
0.201246	0.39685	151760.	RowBox[{-, 80.251}]	RowBox[{-, 6230.45}]	1.60584	0.379274	0	0
0.201246	0.436535	176661.	RowBox[{-, 66.3535}]	RowBox[{-, 7535.4}]	1.68521	0.389911	0	0
0.201246	0.47622	203492.	RowBox[{-, 55.4446}]	RowBox[{-, 9018.02}]	1.76458	0.400252	0	0
0.201246	0.595275	295522.	RowBox[{-, 34.1466}]	RowBox[{-, 14642.7}]	2.00269	0.429734	0	0
0.201246	0.793701	487231.	RowBox[{-, 17.4789}]	RowBox[{-, 28605.9}]	2.39954	0.474748	0	0
0.223607	0.00793701	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	RowBox[{-, 935.393}]	RowBox[{-, 534.535}]	0.872732	RowBox[{RowBox[{0.179292, }], +, RowBox[{0.179292, , i}]}]	0	0
0.223607	0.039685	33313.	RowBox[{-, 769.067}]	RowBox[{-, 650.138}]	0.936228	0.244556	0	0
0.223607	0.0595275	27934.7	RowBox[{-, 672.3}]	RowBox[{-, 743.715}]	0.975913	0.262029	0	0
0.223607	0.0793701	27997.9	RowBox[{-, 584.549}]	RowBox[{-, 855.361}]	1.0156	0.273601	0	0
0.223607	0.198425	56789.9	RowBox[{-, 252.231}]	RowBox[{-, 1982.31}]	1.25371	0.320088	0	0
0.223607	0.23811	71726.6	RowBox[{-, 194.904}]	RowBox[{-, 2565.37}]	1.33308	0.33296	0	0
0.223607	0.31748	107788.	RowBox[{-, 121.68}]	RowBox[{-, 4109.15}]	1.49182	0.356973	0	0
0.223607	0.357165	128798.	RowBox[{-, 98.192}]	RowBox[{-, 5092.06}]	1.57119	0.368308	0	0
0.223607	0.39685	151760.	RowBox[{-, 80.251}]	RowBox[{-, 6230.45}]	1.65056	0.379274	0	0
0.223607	0.436535	176661.	RowBox[{-, 66.3535}]	RowBox[{-, 7535.4}]	1.72993	0.389911	0	0
0.223607	0.47622	203492.	RowBox[{-, 55.4446}]	RowBox[{-, 9018.02}]	1.8093	0.400252	0	0
0.223607	0.595275	295522.	RowBox[{-, 34.1466}]	RowBox[{-, 14642.7}]	2.04741	0.429734	0	0
0.223607	0.793701	487231.	RowBox[{-, 17.4789}]	RowBox[{-, 28605.9}]	2.44426	0.474748	0	0

$RowBox[{stainlesssteel420, , thrust = , , 1000000, , vol in^3 = , , 3294.66}]$

rBot	Wall	stress lbf	sp thrust	weight	dia	r max stress	min # noz	max # noz
0.158114	0.01	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	RowBox[{-, 847.768}]	RowBox[{-, 1179.57}]	0.852348	RowBox[{RowBox[{0.225893, }], +, RowBox[{0.225893, , i}]}]	0	0
0.158114	0.05	33313.	RowBox[{-, 697.168}]	RowBox[{-, 1434.37}]	0.932348	0.308121	0	0
0.158114	0.075	27934.7	RowBox[{-, 610.714}]	RowBox[{-, 1637.43}]	0.982348	0.330136	0	0
0.158114	0.1	27997.9	RowBox[{-, 532.623}]	RowBox[{-, 1877.5}]	1.03235	0.344716	0	0
0.158114	0.25	56789.9	RowBox[{-, 235.257}]	RowBox[{-, 4250.66}]	1.33235	0.403286	0	0
0.158114	0.3	71726.6	RowBox[{-, 183.029}]	RowBox[{-, 5463.6}]	1.43235	0.419504	0	0
0.158114	0.4	107788.	RowBox[{-, 115.534}]	RowBox[{-, 8655.43}]	1.63235	0.449757	0	0
0.158114	0.45	128798.	RowBox[{-, 93.6444}]	RowBox[{-, 10678.7}]	1.73235	0.464038	0	0
0.158114	0.5	151760.	RowBox[{-, 76.8259}]	RowBox[{-, 13016.4}]	1.83235	0.477855	0	0
0.158114	0.55	176661.	RowBox[{-, 63.7314}]	RowBox[{-, 15690.9}]	1.93235	0.491257	0	0
0.158114	0.6	203492.	RowBox[{-, 53.407}]	RowBox[{-, 18724.1}]	2.03235	0.504286	0	0
0.158114	0.75	295522.	RowBox[{-, 33.1137}]	RowBox[{-, 30198.9}]	2.33235	0.541431	0	0
0.158114	1.	487231.	RowBox[{-, 17.0731}]	RowBox[{-, 58571.5}]	2.83235	0.598145	0	0
0.189737	0.01	RowBox[{RowBox[{136383., }], -, RowBox[{77992., , i}]}]	RowBox[{-, 847.768}]	RowBox[{-, 1179.57}]	0.915593	RowBox[{RowBox[{0.225893, }], +, RowBox[{0.225893, , i}]}]	0	0
0.189737	0.05	33313.	RowBox[{-, 697.168}]	RowBox[{-, 1434.37}]	0.995593	0.308121	0	0
0.189737	0.075	27934.7	RowBox[{-, 610.714}]	RowBox[{-, 1637.43}]	1.04559	0.330136	0	0
0.189737	0.1	27997.9	RowBox[{-, 532.623}]	RowBox[{-, 1877.5}]	1.09559	0.344716	0	0
0.189737	0.25	56789.9	RowBox[{-, 235.257}]	RowBox[{-, 4250.66}]	1.39559	0.403286	0	0
0.189737	0.3	71726.6	RowBox[{-, 183.029}]	RowBox[{-, 5463.6}]	1.49559	0.419504	0	0
0.189737	0.4	107788.	RowBox[{-, 115.534}]	RowBox[{-, 8655.43}]	1.69559	0.449757	0	0
0.189737	0.45	128798.	RowBox[{-, 93.6444}]	RowBox[{-, 10678.7}]	1.79559	0.464038	0	0
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0.316228	0.075	27934.7	RowBox[{-, 610.714}]	RowBox[{-, 1637.43}]	1.29858	0.330136	0	0
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Legend

Legend:

text color black -- normal or certain
red -- incomplete or a problem
blue -- probably ok assumptions or design variables
magenta -- not completely certain, but not totally bogus
dark green Key piece of Physics
green -- assumptions or design variables too hard to read
cyan too hard to read
yellow -- unreadable

 MaxMemoryUsed[ ] MemoryInUse[ ]

todonozzle calculate geometrycalcualte geometry of impeller/in ... subtract fromspindleadd hack to rotor spindle to hook it to rotor

RowBox[{{, RowBox[{RowBox[{RowBox[{(, RowBox[{calcualte, , impeller, , of, , RowBox[{(, Row ... RowBox[{(, RowBox[{combustionChamberHeight, , 0.0266592}], )}]}], )}], /, inducer}]}], }}]

$Syntax :: bktmcp : Expression \" (aspiecetosubtractfromspindleaddhackto5spindletohookittorotor\" has no closing \") \". More…$

Created by Mathematica (February 17, 1976)