Preliminary Flight Rating Tests of the hybrid rocket propulsion system for the HAST target missile were accomplished by the Air Force Rocket Propulsion Laboratory. Nine tests of the flight configuration system were conducted at simulated altitude. Overall operating characteristics and performance were shown to be satisfactory for missile flight tests.
Preliminary Flight Rating Tests of the HAST Propulsion System
1975
199 pages
Report
Keine Angabe
Englisch
Rocket Engines & Motors , Hybrid rocket engines , Hybrid propulsion , Aerial targets , Guided missiles , Flight testing , Liquid rocket oxidizers , Solid rocket fuels , Nitric acid , Polybutadiene , Acrylic resins , Fuel systems , Thrust control , Systems engineering , Expulsion , Pressure regulators , Corrosion , Storage , Supersonic aircraft , Pumps , Bearings , Seals , Performance(Engineering) , High altitude , Simulation , Target missiles , High altitude supersonic targets , HAST(High altitude supersonic targets)
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