Millions of lbs of thrust required to launch large space vehicles can be obtained by using large solid-propellant rocket motors; method presented for loading castable solid propellants into large launching units in position at launching sites; include potential site location, motor shell erection, etc.
On-site loading of solid propellants for large missile and satellite launching units
ASME -- Paper
ASME Meeting ; 1959 Launching
American Society of Mechanical Engineers -- Papers ; n 59-AV-19
1959
4 pages
Conference paper
English
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NTIS | 1965
|NTIS | 1964
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