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Isomer Heat Exchanger Combustor Replacement for a Supersonic Ramjet Powered Vehicle Jonathan C. Cox
Isomer Heat Exchanger Combustor Replacement for a Supersonic Ramjet Powered Vehicle
Jonathan C. Cox
This study investigated the possibility of utilizing a Triggered Isomer Heat Exchanger (TIHE) within a ramjet engine to power a supersonic Conventional Air Launched Cruise Missile (CALCM). A computational ramjet engine was created using engine analysis software. This model was then run through a simulated cruise missile mission using AEDsys, a mission analysis and engine performance software suite. The replacement of the combustor with a TIHE led to an impressive range increase for the supersonic cruise missile.
| メディア | 書籍 Paperback Book (ソフトカバーで背表紙を接着した本) |
| リリース済み | 2012年9月20日 |
| ISBN13 | 9781249449607 |
| 出版社 | BiblioScholar |
| ページ数 | 62 |
| 寸法 | 3 × 189 × 246 mm · 127 g |
| 言語 | 英語 |
| 寄稿者 | Air Force Institute of Technology (U.S. |