Path: Orbit/StraightLine
% Power-Limited Rocket Demo For a fixed payload mass and fuel mass, compute the optimal power (engine size) for a mission to 10 AU. Assume engine parameters for specific power and tank fraction. ------------------------------------------------------------------------ See also: SLPLDataStructure, SLPLSolver ------------------------------------------------------------------------
Orbit: StraightLine/SLPLDataStructure Orbit: StraightLine/SLPLSolver Common: Database/Constant Common: Graphics/Plot2D
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