Conceptual study of lunar landing modules

Mathematics – Logic

Scientific paper

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Japanese Spacecraft, Lunar Landing, Lunar Landing Modules, Lunar Landing Sites, Lunar Launch, Lunar Roving Vehicles, Mission Planning, Spacecraft Design, Liquid Hydrogen, Spacecraft Configurations, Spacecraft Guidance, Spacecraft Orbits, Spacecraft Propulsion, Spacecraft Structures, Temperature Control

Scientific paper

An overview of the missions, systems, and subsystems of a lunar rover module, to be launched by the H-2 launch vehicle, is presented. The following topics are discussed: environmental measurement; geological survey of regolith; ground and underground structure surveys; an example of the mission model; the weight and electric power allotments; mission profiles; sequence of events of the landing module; navigation and guidance control; propulsion; thermal control; structure subsystems; landing orbit optimization through the Pontryagin's maximum principle; and an analysis of LH2 evaporation.

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