Path: Interplanetary/Mars
% Mars mission Compute the optimal exhaust velocity for the Mars mission (given the other engine parameters), and the resulting thrust required for the specified payload. See also: StraightLineOptimal, InitialMass, SwitchTime, EngineReport, SimulateStraightLineTrajectory, Straight2DStructure, Constant
StraightLine: ConstantThrust/EngineReport StraightLine: ConstantThrust/InitialMass StraightLine: ConstantThrust/SimulateStraightLineTrajectory StraightLine: ConstantThrust/Straight2DStructure StraightLine: ConstantThrust/StraightLineOptimal StraightLine: ConstantThrust/SwitchTime Common: Database/Constant
Back to the Interplanetary Module page