Path: Propulsion/Utilities
-------------------------------------------------------------------------- The rocket equation including special relativity. Demo is for a boron-proton rocket. Since version 10. -------------------------------------------------------------------------- Form: mR = RocketEquationRelativistic( u, iSp ) -------------------------------------------------------------------------- ------ Inputs ------ u (1,:) Velocity change (km/s) Isp (1,1) Specific impulse (sec) ------- Outputs ------- mR (1,:) Mass ratio final mass/initial mass --------------------------------------------------------------------------
AC: ACData/ACTConstants SC: SCData/sCTConstants Common: CommonData/Constants Common: CommonData/SwooshWatermark Common: CommonData/xSplashSmall Common: Database/Constant Common: General/CellToMat Common: General/DeleteCell Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle
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