Characteristics and important technical advancements; 3 possible solutions of problems in fields of manufacture, transportation and safe handling; building block concept is illustrated and thrust range and burning duration, attained for given chamber diameter under certain conditions, calculated; very large rocket motors up to 1,000,000 lb weight for boosters using concept, offer economical advantages.
Development problems of large solid propellant rocket motors
Entwicklungsprobleme grosser Feststofftriebwerke
Raketentechnik u Raumfahrtforschung ; 5 , n 1
1961
8 pages
Aufsatz (Zeitschrift)
Deutsch
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