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Chemical, Electric, Gas, Help, Nuclear, PropulsionData, Rocket, Utilities, Demos/Chemical, Demos/Rocket, Demos/Utilities,
Fuels - Computes molecular weight, ratio of specific heats and gas constant for
QRFuel - The lower heating value for fuels.
QRHydrocarbon - The lower heating value for a hydrocarbon fuel.
QRHydrogen - The lower heating value for H2 + 1/2O2 -> H20.
AtomicMass - Outputs atomic mass.
EVToV - Convert electron volts to velocity.
ElectricPropulsion - Design a electric powered transfer vehicle.
ElectricPropulsionDesign - Design an electric propulsion system.
FElectricPropulsion - Computes the total mass, fuel mass and power for an electric thruster.
FMinUE - Function to be minimized by OptimalVehicle.m
HallThrusterArray - Create a PPPL Hall thruster array picture.
KEVToJ - Convert keV to J.
OptimalVehicle - Finds the optimal vehicle given various parameters. The routine takes
TElec - Computes the thrust and specific impulse of an electric thruster.
TVDesign - Design an electric transfer vehicle.
VToEV - Convert velocity to electron volts.
AreaRatioFromMach - Computes the area ratio from Mach Number.
BloDownMass - Generates a blowdown curve of mass vs. pressure.
CombTemp - Computes the combustion temperature of a gas mixture.
Gamma - Computes the ratio of specific heats of a gas mixture.
GasMass - Generates a blowdown curve of mass vs. pressure.
GasProperties - Returns gas properties.
IsentropicExpansion - Computes isentropic expansion.
MachFromAreaRatio - Computes the Mach number from area ratio. The throat is at Mach 1.
MachNumber - Compute the Mach number
MolWt - Computes the molecular weight of a gas mixture.
SpeedSnd - Compute the speed of sound.
VolumeToPressureBD - Generates the final pressure
FileHelp - View the file headers.
NuclearThermalUE - Compute the exhaust velocity for a nuclear rocket with H2 fuel.
ColdGas - Determines performance of a cold gas rocket.
IdealRkt - Computes the thrust and exhaust velocity for an ideal rocket. p0 or e may be
Isp2V - Compute specific impulse from exhaust velocity
Plume - Compute the plume forces and torques on a set of elemental areas.
RocketH2 - Computes the thrust and exhaust velocity of an H2 rocket.
SolidR - Computes the right hand side of the dynamical equations for a solid
TCoeff - Computes the ideal thrust coefficient for a nozzle with a diverging portion.
UE - Computes the ideal exhaust velocity of a rocket.
UEO2H2 - Computes the exhaust velocity of a O2/H2 rocket.
UEQR - Computes the exhaust velocity of a rocket from fuel lower heating
V2Isp - Compute specific impulse from exhaust velocity
VolumeToDimension - Computes the dimensions of a tank. Four types may be entered:
SphericalTankFluidHeight - Compute the height of fuel in a spherical fuel tank.
ThrusterLayout - Tool for thruster layout.
TBlodown - Demonstrate blow down. Most satellites use unregulated blowdown systems.
TSolid - Demonstrate a solid rocket motor.
SRTPropulsionDesign - Design the propulsion system for SRT-M
SVN Revision: 23297
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