| タイトル | Reusable Agena study. Volume 2: Technical |
| 本文（外部サイト） | http://hdl.handle.net/2060/19740024172 |
| 著者（英） | Carter, W. K.; Fitzgerald, E. T.; Douglass, D. A.; Jensen, H. L.; Hopkins, C. V.; Sagawa, S. S.; Carter, S. A.; Waller, E. W.; Piper, J. E. |
| 著者所属（英） | Lockheed Missiles and Space Co. |
| 発行日 | 1974-03-15 |
| 言語 | eng |
| 内容記述 | The application of the existing Agena vehicle as a reusable upper stage for the space shuttle is discussed. The primary objective of the study is to define those changes to the Agena required for it to function in the reusable mode in the 100 percent capture of the NASA-DOD mission model. This 100 percent capture is achieved without use of kick motors or stages by simply increasing the Agena propellant load by using optional strap-on-tanks. The required shuttle support equipment, launch and flight operations techniques, development program, and cost package are also defined. |
| NASA分類 | SPACE VEHICLES |
| レポートNO | 74N32285
NASA-CR-120362
LMSC-D383059-VOL-2 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/193155 |
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