| タイトル | Performance assessment of aero-assisted orbital transfer vehicles |
| 本文（外部サイト） | http://hdl.handle.net/2060/19850008684 |
| 著者（英） | Arrington, J. P.; Mccandless, R. S.; Wilhite, A. W.; White, N. H.; Rehder, J. J.; Stone, H. W.; Powell, R. W.; Talay, T. A.; Naftel, J. C. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1984-04-01 |
| 言語 | eng |
| 内容記述 | Aero-assisted orbital transfer vehicles are analyzed. The aerodynamic characteristics over the flight profile and three- and six-degree-of-freedom performance analyses were determined. The important results, to date, are: (1) the aerodynamic preliminary analysis system, an interactive computer program, used to predict the aerodynamics (performance, stability, and control) for these vehicles; (2) the performance capability, e.g., maximum inclination change, maximum heating rate, and maximum sensed acceleration, can be determined using continuum aerodynamics only; (3) guidance schemes can be developed that allow for errors in atmospheric density prediction, mispredicted trim angle of attack, and off-nominal atmospheric interface conditions, even for vehicles with a low lift-to-drag ratio; and (4) multiple pass trajectories can be used to reduce the maximum heating rate. |
| NASA分類 | LAUNCH VEHICLES AND SPACE VEHICLES |
| レポートNO | 85N16993 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/567026 |
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