Report of work in progress at Rocket Propulsion Establishment (RPE) of Ministry of Aviation; text and photographs refer to fan spray fuel injector, 4000 lb thrust liquid oxygen/liquid hydrogen engine, 137,000 lb thrust RZ-2 Rolls Royce engine, 585,000 lb sec total impulse dual thrust solid propellant motor, etc. (See also Engineer v 217 n 5655 June 12 1964 p 1023-5)
British rocket research
Engineering
Engineering ; 197 , n 5122
1964
2 pages
Aufsatz (Zeitschrift)
Englisch
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