1. Avery successful development program of scramjet-powered missiles for fleet defense was carried out during the period 1961-1978. Con
2. distributionalongSCRAMengine modulecenterllne. the components verified the methods that were used. The components were successfully integrated into a viable engine design and tests of the engine in freejets at Mach 5 - 7.2 clearly demonstrated the feasibility of liquid fueled scramjet engines. Some of the highlights of the test program and analysis thereof are:
3. Serafini,J.S., Dorsch, R.G., and Fletcher, E.A. "Exploratory Investigation of Staticand Base-Pressure Increases Resulting from Combustion of Aluminum Borohydride Ad.jacent to Body of Revolution in Supersonic Wind Tunnel,"NACA RM E57E15 (October 1957)