Path: Orbit/OrbitManeuver
% Delta-V for a Hohmann transfer between LEO and GEO. Start in a 200 km circular 9.1 deg orbit. The initial orbit and transfer orbit mass are acheivable by a Falcon 1e rocket. The Falcon 1e can lift smaller masses into higher orbits so this is not necessarily the best you can do with the Falcon 1e. Since version 8. ------------------------------------------------------------------------ See also OrbMnvrInclAndHohm and RocketMass. ------------------------------------------------------------------------ % ------------------------------------------------------------------------------- Copyright (c) 2009 Princeton Satellite Systems, Inc. All rights reserved. -------------------------------------------------------------------------------
Orbit: OrbitManeuver/OrbMnvrInclAndHohm Propulsion: Rocket/RocketMass 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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