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Path: SC/Demos/CAD
% Generates a lunar module model.
This combines the ascent and descent vehicles.
Data:
CSM Orbit 54 x 66 nm lunar orbit
LM does delta-V to an 8 by 60 nm elliptical orbit
Contact probes are 68 inches
the weight breakdown is as follows:
Ascent stage, dry 4,804 lb Includes water and oxygen; no crew
Descent stage, dry 4,483 lb
RCS propellants (loaded) 604 lb
DPS propellants (loaded) 18,100 lb
APS propellants (loaded) 5,214 lb
Total weight 33,205 lb
Engine 6 deg gimbal to handle ACS and CM offset
Engine throttle between 1050 and 6300 lbf Max thrust is 9,870 lbf
RCS 100 lb thrust
Aerozine 50 and nitrogen tetroxide.
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See also BuildCADModel, CreateBody, CreateComponent, Inertias,
LunarModuleFirstStage, LunarModuleSecondStage, Constant
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%
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Copyright (c) 2002 Princeton Satellite Systems, Inc.
All rights reserved.
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AeroUtils: CAD/BuildCADModel AeroUtils: CAD/CreateBody AeroUtils: CAD/CreateComponent AeroUtils: ComponentModels/LunarModuleFirstStage AeroUtils: ComponentModels/LunarModuleSecondStage Common: Database/Constant Common: Graphics/DrawCAD Common: MassProperties/Inertias
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