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.


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    Flight Tests of Exhaust-Gas Jet Propulsion

    B. Pinkel / L. R. Turner | NTIS | 1940


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    Pinkel, B. / Turner, L.R. | Engineering Index Backfile | 1940


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