Path: Interplanetary/InterplanetaryOrbit
% Interstellar mission simulation with a sun gravity assist. The spacecraft is put into an elliptical orbit with a near sun perigee. Near perigee a high-power plasma thruster performs a delta-V. The delta-V is amplified by the sun's gravity well. Since version 2. ------------------------------------------------------------------------ See also Constant, TextS, TitleS, XLabelS, YLabelS, RK4, RARP2A, Period, VOrbit, FHel ------------------------------------------------------------------------ % --------------------------------------------------------------------------- Copyright 1998 Princeton Satellite Systems, Inc. All rights reserved. ---------------------------------------------------------------------------