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: Straight2DStructure, TOFConstThrust, EngineReport, SimulateStraightLineTrajectory
StraightLine: ConstantThrust/EngineReport StraightLine: ConstantThrust/SimulateStraightLineTrajectory StraightLine: ConstantThrust/Straight2DStructure StraightLine: ConstantThrust/TOFConstThrust Common: Database/Constant
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