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.
Isomer Heat Exchanger Combustor Replacement for a Supersonic Ramjet Powered Vehicle
2004
59 pages
Report
Keine Angabe
Englisch
Ramjet-powered supersonic transports
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