| タイトル | OVRhyp, Scramjet Test Aircraft |
| 本文（外部サイト） | http://hdl.handle.net/2060/19910000728 |
| 著者（英） | Bisard, T.; Peters, W.; Hufford, G.; Draper, K.; Dallinga, S.; Rogers, J.; Aslan, J. |
| 著者所属（英） | Universities Space Research Association; Ohio State Univ. |
| 発行日 | 1990-05-01 |
| 言語 | eng |
| 内容記述 | A preliminary design for an unmanned hypersonic research vehicle to test scramjet engines is presented. The aircraft will be launched from a carrier aircraft at an altitude of 40,000 feet at Mach 0.8. The vehicle will then accelerate to Mach 6 at an altitude of 100,000 feet. At this stage the prototype scramjet will be employed to accelerate the vehicle to Mach 10 and maintain Mach 10 flight for 2 minutes. The aircraft will then decelerate and safely land. |
| NASA分類 | AIRCRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 91N10041
NASA-CR-187009
NAS 1.26:187009 |
| 権利 | No Copyright |
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