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 Engineering v 197 n 5122 June 19 1964 p 842-3)
British rocket research
Engineer
Engineer ; 217 , n 5655
1964
3 pages
Aufsatz (Zeitschrift)
Englisch
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