| タイトル | Advanced hypersonic aircraft design |
| 本文（外部サイト） | http://hdl.handle.net/2060/19930008848 |
| 著者（英） | Harvey, Greg; Utzinger, Rob; Nagy, Greg; Molnar, Dave; Petersen, Steve; Blank, Hans-Joachim; Cox, Craig; Mckee, Mike |
| 著者所属（英） | Ohio State Univ. |
| 発行日 | 1992-06-01 |
| 言語 | eng |
| 内容記述 | The objective of this design project is to develop the hypersonic reconnaissance aircraft to replace the SR-71 and to complement existing intelligence gathering devices. The initial design considerations were to create a manned vehicle which could complete its mission with at least two airborne refuelings. The aircraft must travel between Mach 4 and Mach 7 at an altitude of 80,000 feet for a maximum range of 12,000 nautical miles. The vehicle should have an air breathing propulsion system at cruise. With a crew of two, the aircraft should be able to take off and land on a 10,000 foot runway, and the yearly operational costs were not to exceed $300 million. Finally, the aircraft should exhibit stealth characteristics, including a minimized radar cross-section (RCS) and a reduced sonic boom. The technology used in this vehicle should allow for production between the years 1993 and 1995. |
| NASA分類 | AIRCRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 93N18037
NASA-CR-192046
NAS 1.26:192046 |
| 権利 | No Copyright |
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