Selfigniting hybrid rocket propellant system employing 90% hydrogen peroxide as oxidizer and polyethylene as fuel; reasoning which led to this choice and advantages achieved; results obtained in tests with one type of fuel charge; qualitative discussion on operation.
Solid-liquid rocket propellant system
Jet Propulsion
Jet Propulsion ; 26 , n 11
1956
4 pages
Article (Journal)
English
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