| タイトル | Lifetimes of lunar satellite orbits |
| 本文（外部サイト） | http://hdl.handle.net/2060/19940023268 |
| 著者（英） | Meyer, Kurt W.; Buglia, James J.; Desai, Prasun N. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1994-03-01 |
| 言語 | eng |
| 内容記述 | The Space Exploration Initiative has generated a renewed interest in lunar mission planning. The lunar missions currently under study, unlike the Apollo missions, involve long stay times. Several lunar gravity models have been formulated, but mission planners do not have enough confidence in the proposed models to conduct detailed studies of missions with long stay times. In this report, a particular lunar gravitational model, the Ferrari 5 x 5 model, was chosen to determine the lifetimes for 100-km and 300-km perilune altitude, near-circular parking orbits. The need to analyze orbital lifetimes for a large number of initial orbital parameters was the motivation for the formulation of a simplified gravitational model from the original model. Using this model, orbital lifetimes were found to be heavily dependent on the initial conditions of the nearly circular orbits, particularly the initial inclination and argument of perilune. This selected model yielded lifetime predictions of less than 40 days for some orbits, and other orbits had lifetimes exceeding a year. Although inconsistencies and limitations are inherent in all existing lunar gravity models, primarily because of a lack of information about the far side of the moon, the methods presented in this analysis are suitable for incorporating the moon's nonspherical gravitational effects on the preliminary design level for future lunar mission planning. |
| NASA分類 | ASTRODYNAMICS |
| レポートNO | 94N27771
NASA-TP-3394
L-17264
NAS 1.60:3394 |
| 権利 | No Copyright |
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