Path: Propulsion/Rocket
% Compute specific impulse from exhaust velocity Since version 1. -------------------------------------------------------------------------- Form: iSP = V2Isp( v, g ) -------------------------------------------------------------------------- ------ Inputs ------ v (1,:) Exhaust velocity g (1,1) Acceleration of gravity (9.806 m/sec^2) ------- Outputs ------- iSP (1,:) Specific impulse (sec) --------------------------------------------------------------------------
Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle
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