Problems in meeting basic requirements of efficient conversion of chemical energy locked up in propellants into kinetic energy to supply useful thrust with least possible weight and greatest possible reliability; their effects on range or altitude which can be achieved. (see also Flight v 69 n 2460 Mar 16 1956 p 299-300)
Combustion chambers for rocket engines
Brit Interplanetary Soc -- J
British Interplanetary Society -- Journal ; 15 , n 3
1956
18 pages
Article (Journal)
English
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Combustion chambers for rocket engines
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