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 Brit Interplanetary Soc -- J v 15 n 3 May-June 1956 p 146-63)
Combustion chambers for rocket engines
Flight
Flight ; 69 , n 2460
1956
2 pages
Article (Journal)
English
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