The heavyweight motor development, the lightweight motor design and the propellant re-evaluation were completed. The final heavyweight motor test results are presented along with the data plots and photographs. The motor was fired at simulated altitude and successfully extinguished.
Feasibility Demonstration of a Single-Chamber Controllable Solid Rocket Motor
1966
106 pages
Report
No indication
English
Rocket Engines & Motors , Rocket Propellants , Solid propellant rocket engines , Controllable-thrust rocket motors , Research management , Design , Solid rocket propellants , Captive tests , Performance(Engineering) , High altitude , Simulation , Rocket components , Feasibility studies , Pressure , Feedback , Test equipment , Diffusers , Control systems , Engine control systems , Pintle nozzles. s/l change 8611