Twenty-eight inch, 700 lb, fiberglass encased rocket engine having capability of putting 200 lb payload into 300 nautical mi circular orbit is described; performance and environmental requirements; design, case manufacture, insulation, nozzle, and propellant are discussed.
Solid propellent motor for third stage of satellite launcher
Spaceflight
Spaceflight ; 9 , n 4
1967
3 pages
Aufsatz (Zeitschrift)
Englisch
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