Engine for ballistic missile applications weighing up to 10,000 lb examined to see whether increase in size by factor of 10 introduces new problems; cartridge loading and case bonding; geometry of propellant; relation of propellant surface to progression of burning and compensation of final surface by slotted charge; transportation problem.
Old problems for big solid rockets
Astronautics
Astronautics ; 3 , n 9
1958
Article (Journal)
English
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Ignition Problems in Solid-Propellant Rockets
NTRS | 1968
|Online Contents | 2012
Online Contents | 1995
Online Contents | 2011
Engineering Index Backfile | 1957
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