The APL Propulsion Research Laboratory constitutes a versatile blowdown facility for the implementation of exploratory development of advanced propulsion systems. Because of its ability to simulate the environmental conditions of high-speed flight, the facility has also been extended to implement experiments on ablation, heat transfer, and wake studies associated with missile re-entry. This is the first of what is intended to be a series of annual progress reports; it covers the period of October 1, 1963 until September 30, 1964. (Author)
Propulsion Research Laboratory Summary Report for FY 1964
1965
65 pages
Report
Keine Angabe
Englisch
Fluid Mechanics , Management Practice , Laboratory & Test Facility Design & Operation , Naval research , Research management , Laboratories , Arc heaters , Thrust augmentation , Combustion , Hypersonic wind tunnels , Supersonic flow , Scheduling , Budgets , Ablation , Heat transfer , Test facilities , Atmosphere entry , Environmental tests , Safety , Test equipment , Instrumentation , Polaris , Scram
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