| タイトル | Lunar Get Away Special (GAS) spacecraft |
| 著者（英） | Salazar, R. P.; Aston, G.; Nock, K. T.; Stella, P. M. |
| 著者所属（英） | Jet Propulsion Lab., California Inst. of Tech. |
| 発行日 | 1987-05-01 |
| 言語 | eng |
| 内容記述 | A new approach to the resumption of Lunar missions is discussed which relies upon Shuttle Get-Away-Special Canisters for launch and solar electric ion propulsion for slow orbit transfer to low Lunar orbit. The technique of orbit transfer is outlined along with a summary of a mission profile for a first mission which could carry a Gamma Ray Spectrometer. System design constraints are discussed followed by a description of the low mass spacecraft concept which has been developed. Particular emphasis is placed upon describing the small solar electric, xenon ion propulsion system. |
| NASA分類 | SPACECRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 87A39632
AIAA PAPER 87-1051 |
| 権利 | Copyright |
