A preliminary design of a lunar landing and launch facility for a Phase 3 lunar base is formulated. A single multipurpose vehicle for the lunar module is assumed. Three traffic levels are envisioned: 6, 12, and 24 landings/launches per year. The facility is broken down into nine major design items. A conceptual description of each of these items is included. Preliminary sizes, capacities, and/or other relevant design data for some of these items are obtained. A quonset hut tent-like structure constructed of aluminum rods and aluminized mylar panels is proposed. This structure is used to provide a constant thermal environment for the lunar modules. A structural design and thermal analysis is presented. Two independent designs for a bridge crane to unload/load heavy cargo from the lunar module are included. Preliminary investigations into cryogenic propellant storage and handling, landing/launch guidance and control, and lunar module maintenance requirements are performed. Also, an initial study into advanced concepts for application to Phase 4 or 5 lunar bases has been completed in a report on capturing, condensing, and recycling the exhaust plume from a lunar launch.
Lunar Landing and Launch Facilities and Operations
1988
203 pages
Report
Keine Angabe
Englisch
Space Launch Vehicles & Support Equipment , Composite Materials , Structural Analyses , Structural Mechanics , Launching bases , Lunar bases , Lunar surface , Planetary landing , Space erectable structures , Cranes , Cryogenic rocket propellants , Design analysis , Lunar module , Maintenance , Storage tanks , Structural analysis , Thermal analysis
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