It is first necessary to decide on duration, thrust, and combustion chamber pressure of motor, and on propellants; main components considered in turn; pumps and turbine should be designed together; impulse turbines and high speed centrifugal pumps are almost invariably used; importance of avoiding cavitation; method by which shape and size of combustion chamber may be determined, also chamber wall thickness; injectors, igniters and valves.
Design of rocket motors
Brit Interplanetary Soc -- J
British Interplanetary Society -- Journal ; 11 , n 3
1952
16 pages
Article (Journal)
English
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Engineering Index Backfile | 1949
|NTIS | 1993
|Engineering Index Backfile | 1947
|Emerald Group Publishing | 1947
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