Propellant requirements for military, commercial and research rocket; how to make usable propellants that do not meet freezing point requirements by use of additives such as ammonium thiocyanate added to hydrazine or water to hydrogen peroxide; nontoxic requirements; size of combustion chamber and injection arrangement; high thermal stability; approximate qualities of some of today's propellants.
Liquid propellants for manned rocket aircraft
Missiles Rockets
Missiles and Rockets ; 2 , n 9
1957
Aufsatz (Zeitschrift)
Englisch
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Engineering Index Backfile | 1957
|UK MANNED ROCKET AIRCRAFT - Papers Presented
Online Contents | 2002
UK MANNED ROCKET AIRCRAFT - The Screamer Rocket Engine
Online Contents | 2002
|LIQUID ROCKET PROPULSION APPLIED TO MANNED AIRCRAFT - IN HISTORICAL PERSPECTIVE
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|Investigation of Liquid Rocket Propellants
NTIS | 1956
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