Background and features of system in which tanks are pressurized by means of solid propellant charge, and combined with combustion chamber to form single package in which propellants are self-igniting; principal characteristics such as resistance to environmental conditions; design problems and possible developments with regard to selection of propellants, materials, burning time, ignition and combustion, and safety; possible applications related to missiles, aircraft, and space projects.
Packaged liquid rocket motors
Roy Aeronautical Soc -- J
Royal Aeronautical Society -- Journal ; 66 , n 615
1962
6 pages
Aufsatz (Zeitschrift)
Englisch
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