| タイトル | Aerothermodynamic heating and performance analysis of a high-lift aeromaneuvering AOTV concept |
| 著者（英） | Wilson, J. F.; Davies, C. B.; Menees, G. P.; Brown, K. G. |
| 著者所属（英） | NASA Ames Research Center; Informatics General Corp. |
| 発行日 | 1985-06-01 |
| 言語 | eng |
| 内容記述 | The thermal-control requirements for design-optimized aeromaneuvering performance are determined for space-based applications and low-earth orbit sorties involving large, multiple plane-inclination changes. The leading-edge heating analysis is the most advanced developed for hypersonic-rarefied flow over lifting surfaces at incidence. The effects of leading-edge bluntness, low-density viscous phenomena, and finite-rate flow-field chemistry and surface catalysis are accounted for. The predicted aerothermodynamic heating characteristics are correlated with thermal-control and flight-performance capabilities. The mission payload capability for delivery, retrieval, and combined operations is determined for round-trip sorties extending to polar orbits. Recommendations are given for future design refinements. The results help to identify technology issues required to develop prototype operational systems. |
| NASA分類 | LAUNCH VEHICLES AND SPACE VEHICLES |
| レポートNO | 85A37674
AIAA PAPER 85-1060 |
| 権利 | Copyright |
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