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. --------------------------------------------------------------------------