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- W51103003 abstract "Abstract : The Aerojet Solid Propulsion Company Modified, full-scale, heavyweight, Controllable Solid Rocket Motor (CSRM-4), was successfully test fired at simulated pressure altitude in Rocket Development Test Cell J-5 of the Engine Test Facility, AEDC, on June 25, 1973. The primary test objective, propellant extinguishment, was demonstrated on five repetitive programmed firings; the five 5-sec duration firings were separated by 60-sec extinguished coast periods. Motor chamber pressure at propellant extinguishment was 36, 26, 32, 30, and 26 psia for the five firings. Postfire condition of the motor was satisfactory." @default.
- W51103003 created "2016-06-24" @default.
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- W51103003 date "1973-11-01" @default.
- W51103003 modified "2023-09-26" @default.
- W51103003 title "Altitude Test of the Aerojet Modified Heavyweight Full-Scale Controllable Solid-Propellant Rocket Motor (CSRM-4)" @default.
- W51103003 hasPublicationYear "1973" @default.
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