| タイトル | Hypersonic airbreathing vehicle conceptual design (focus on aero-space plane) |
| 本文（外部サイト） | http://hdl.handle.net/2060/19890015839 |
| 著者（英） | Hunt, James L.; Martin, John G. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1989-04-01 |
| 言語 | eng |
| 内容記述 | The airbreathing single stage to orbit (SSTO) vehicle design environment is variable-rich, intricately networked and sensitivity intensive. As such, it represents a tremondous technology challenge. Creating a viable design will require sophisticated configuration/synthesis and the synergistic integration of advanced technologies across the discipline spectrum. In design exercises, reductions in the fuel weight-fraction requirements projected for an orbital vehicle concept can result from improvements in aerodynamics/controls, propulsion efficiencies and trajectory optimization; also, gains in the fuel weight-fraction achievable for such a concept can result from improvements in structural design, heat management techniques, and material properties. As these technology advances take place, closure on a viable vehicle design will be realizable. |
| NASA分類 | AIRCRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 89N25210 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/141569 |
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