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Isomer Heat Exchanger Combustor Replacement for a Supersonic Ramjet Powered Vehicle Jonathan C. Cox
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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.
| Medios de comunicación | Libros Paperback Book (Libro con tapa blanda y lomo encolado) |
| Publicado | 20 de septiembre de 2012 |
| ISBN13 | 9781249449607 |
| Editores | BiblioScholar |
| Páginas | 62 |
| Dimensiones | 3 × 189 × 246 mm · 127 g |
| Lengua | Inglés |
| Colaborador | Air Force Institute of Technology (U.S. |
