| タイトル | Hypersonic research engine/aerothermodynamic integration model: Experimental results. Volume 3: Mach 7 component integration and performance |
| 本文（外部サイト） | http://hdl.handle.net/2060/19760016172 |
| 著者（英） | Andrews, E. H., Jr.; Mackley, E. A. |
| 著者所属（英） | AiResearch Mfg. Co.|NASA Langley Research Center |
| 発行日 | 1976-04-01 |
| 言語 | eng |
| 内容記述 | The NASA Hypersonic Research Engine Project was undertaken to design, develop, and construct a hypersonic research ramjet engine for high performance and to flight test the developed concept on the X-15-2A airplane over the speed range from Mach 3 to 8. Computer program results are presented here for the Mach 7 component integration and performance tests. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 76N23260
NASA-TM-X-72823 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/185962 |
