| タイトル | Common lunar lander |
| 著者（英） | Hyatt, C. D.; Culpepper, W.; Bailey, S.; Kluksdahl, E.; Pelischek, T.; Pruett, D.; Stecklein, J.; Wagner, L.; Rickman, S.; Chen, H. |
| 著者所属（英） | NASA Johnson Space Center |
| 発行日 | 1992-03-01 |
| 言語 | eng |
| 内容記述 | 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. |
| NASA分類 | LAUNCH VEHICLES AND SPACE VEHICLES |
| レポートNO | 92A38600
AIAA PAPER 92-1481 |
| 権利 | Copyright |
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