The Air Force and NASA share a common interest in developing advanced propulsion systems for commercial and military aerospace vehicles which require efficient acceleration and cruise operation in the Mach 4 to 6 flight regime. The principle engine of interest is the turboramjet; however, other combined cycles such as the turboscramjet, air turborocket, supercharged ejector ramjet, ejector ramjet, and air liquefaction based propulsion are also of interest. Over the past months careful planning and program implementation have resulted in a number of development efforts that will lead to a broad technology base for those combined cycle propulsion systems. Individual development programs are underway in thermal management, controls materials, endothermic hydrocarbon fuels, air intake systems, nozzle exhaust systems, gas turbines and ramjet ramburners.
Airbreathing Combined Cycle Engine Systems
1992
9 pages
Report
Keine Angabe
Englisch
Rocket Engines & Motors , Propulsion system configurations , Turboramjet engines , Turborocket engines , Air breathing engines , Propulsion system performance , Aerospace vehicles , Air intakes , Ejectors , Endothermic fuels , Exhaust systems , Hydrocarbon fuels , Intake systems , Liquefaction , Supersonic speed , Temperature control
Airbreathing combined cycle engine systems
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