Path: Propulsion/Demos/Chemical

% Design a propulsion system for a low-earth orbit satellite
 We assume a constant orbit for drag purposes. You can add any number
 of Hohmann transfers and any number of phase changes. You can add other
 maneuvers to this script.

 We assume a blowdown system with helium as the pressurant.
 The momentum calculations assume a fixed center-of-mass offset.
 If one thruster overwhelms the RWA capacity it recommends a 4 thruster
 configuration. In that case you use off-pulsing during maneuvers.

 See also OrbMnvrHohmann, OrbMnvrPhaseChange, DVOrbitDrag, RocketMass, 
 BDDesign, Period, Constant, CreateLatexTable, DisplayLatexTable


Common: Database/Constant
Common: General/CreateLatexTable
Common: General/DisplayLatexTable
Orbit: OrbitManeuver/OrbMnvrHohmann
Orbit: OrbitManeuver/OrbMnvrPhaseChange
Orbit: OrbitMechanics/DVOrbitDrag
Propulsion: Rocket/RocketMass
SC: Actuator/BDDesign
SC: BasicOrbit/Period

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