Path: Orbit/OrbitManeuver
% Computes a preliminary design of a two stage to orbit vehicle. It computes the delta-V required given an initial velocity (Mach 6 at 30 km) ------------------------------------------------------------------------- See also LambertTOF, AtmDens2, Plot2D, Mag ------------------------------------------------------------------------- % -------------------------------------------------------------------------- Copyright 1995-1998 Princeton Satellite Systems, Inc. All rights reserved. --------------------------------------------------------------------------
Toolboxes: SourceCode/LambertTOF AerospaceUtils: AtmosphericCalculations/AtmDens2 Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/DeBlankLT Common: General/DispWithTitle Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Common: Graphics/TitleS Common: Graphics/XLabelS Common: Graphics/YLabelS Math: Linear/Cross Math: Linear/Mag Math: Linear/Unit
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