| タイトル | An estimate of the global minimum DV needed for earth-moon transfer |
| 著者（英） | Sweetser, Theodore H. |
| 著者所属（英） | Jet Propulsion Lab., California Inst. of Tech. |
| 発行日 | 1991-01-01
1991 |
| 言語 | eng |
| 内容記述 | An estimate is found for a lower bound on the Delta V needed for any trajectory which starts at 167 km altitude circular earth orbit and ends in a 100 km altitude circular polar lunar orbit. The analysis used involves calculations of Jacobi's integral in a circular restricted three-body problem which approximates the earth-moon transfer problem. The result is an estimate that any such trajectory will require Delta Vs of at least 3099 km/s to leave the neighborhood of earth and at least 0.622 km/s to achieve the desired orbit around the moon, for a total of 3721 km/s. |
| NASA分類 | ASTRODYNAMICS |
| レポートNO | 93A17909
AAS PAPER 91-101 |
| 権利 | Copyright |
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