Common lunar lander

Details Common lunar lander Common lunar lander

Mar 1992

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1992aiaa.conft....b&link_type=abstract

AIAA, Space Programs and Technologies Conference, Huntsville, AL, Mar. 24-27, 1992. 19 p.

Computer Science

Performance

Lunar Landing, Lunar Orbits, Lunar Surface, Mission Planning, Nasa Space Programs, Launch Vehicles, Orbit Insertion, Temperature Control

Scientific paper

This report focuses on the reference lander design developed at the Johnson Space Center, describing a small lunar soft lander with the capability to soft land about 64 kilograms of payload at any lunar latitude and longitude. The Artemis lander is a sun-pointing, three-axis vehicle that contributes to the translunar injection burn and performs the lunar orbit insertion, deorbit, descent and landing maneuvers with a single liquid bipropellant lander stage. Attention is given to mission profile and performance, the guidance, navigation and control subsystem, the propulsion subsystem, and the flight data subsystem.

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