Chemical, Electric, LVModels, MultiStage, Nuclear, Rocket, Demos/Chemical, Demos/LVModels, Demos/MultiStage, Demos/Rocket,
BloDownMass - Generates a blowdown curve of mass vs. pressure.
ColdGas - Determines performance of a cold gas rocket.
CombTemp - Computes the combustion temperature of a gas mixture.
Fuels - Computes molecular weight, ratio of specific heats and gas constant for
Gamma - Computes the ratio of specific heats of a gas mixture.
GasMass - Generates a blowdown curve of mass vs. pressure.
MachNo - Compute the Mach number
MolWt - Computes the molecular weight of a gas mixture.
SolidR - Computes the right hand side of the dynamical equations for a solid
SpeedSnd - Compute the speed of sound.
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.
VolumeToPressureBD - Generates the final pressure
AtomicMass - Outputs atomic mass.
EVToV - Convert electron volts to velocity.
ElectricPropulsion - Design a electric powered transfer vehicle.
ElectricPropulsionDesign - Design an electric propulsion system.
FElectricPropulsion - f( nargin < 1 )
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.
FMinTOrbitInjection - Function to be minimized by fmins for MinTOrbitInjection.
LaunchParamToEl - Converts flight path angle, velocity and r to orbital elements.
LaunchVehicle2D - The right hand side of a 2D launch model.
LaunchVehicle3D - Compute position, velocity and mass derivatives for a launch vehicle.
MinTOrbitInjection - Constant thrust minimum time orbit injection.
RHSMinTOrbitInjection - RHS for planar equations.
Reentry - Non dimensional reentry dynamics model.
ReentryPlot - Plot values from reentry simulations.
BurnoutVelocity - Compute the burnout velocity for a multi-stage rocket
EP2M - Converts structural and payload ratios into masses.
EPPS - Payload and structural mass ratios for parallel stages.
M2EP - Converts masses to structural and payload ratios.
M2MS - Converts total, final and payload masses to stage masses and ratios.
MS2M - Converts stage and payload masses to total masses and final masses.
MSData - Complete the stage data for a multi-stage missile.
MSTOR - Computes the multistage tradeoff ratios.
MSVRatio - Compute the velocity ratio for a multi-stage rocket
OptimalPayloadRatio - Compute the optimal payload ratios for a multi-stage rocket.
SS2O - Compute the fuel mass needed to reach a velocity given mass properties and ISP.
NuclearThermalUE - Compute the exhaust velocity for a nuclear rocket with H2 fuel.
IdealRkt - Computes the thrust and exhaust velocity for an ideal rocket. p0 or e may be
Isp2V - Compute specific impulse from exhaust velocity
MissileDistance - Compute the min angular distance (around the Earth) that connects 2 pts
MissileLambert - Find initial velocity and flight path angle that gives desired distance
MissileMaxRange - Compute the maximum range for a missile given its initial velocity.
MissileTrajAnalysis - Analyze the trajectories for around-the-Earth missile launches.
MissileVelocity - Compute initial velocity and flight time for a missile trajectory
Plume - Compute the plume forces and torques on a set of elemental areas.
RocketDatabase - Load the properties for a rocket: mS, thrust, ISP, exhaust velocity.
RocketFuelMass - Compute the fuel mass required to reach a burnout velocity (single-stage)
V2Isp - Compute specific impulse from exhaust velocity
VolumeToDimension - Computes the dimensions of a tank. Four types may be entered:
TBlodown - Demonstrate blow down. Most satellites use unregulated blowdown systems.
TSolid - Demonstrate a solid rocket motor.
ISSMission - Explore different launch vehicles for an ISS orbit
LaunchSimulation - Launch vehicle simulation.
ReentryCartSimulation - Reentry simulation.
ReentrySimulation - Launch vehicle simulation for an SSTO vertical launch.
SSTO3DLaunchSimulation - Launch vehicle simulation for an SSTO vertical launch.
SSTOLaunchSimulation - Launch vehicle simulation for an SSTO vertical launch.
SolveGravityTurn - Solve for the initial conditions to perform a gravity turn trajectory.
TLunarT - Plan a simplified lunar transfer assuming you start in a geo transfer
SVN Revision: 10554
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