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.
Common lunar lander
01.03.1992
Aufsatz (Konferenz)
Keine Angabe
Englisch
AIAA | 1992
|Common Lunar Lander (CLL) Propulsion System
NTIS | 1991
|Artemis: Common Lunar Lander Project Status
NTIS | 1992
|Common Lunar Lander (CLL) Trajectory Analysis
NTIS | 1991
|Design of a Common Lunar Lander
NTIS | 1991
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