A review is given of the performance of 98 percent H2O2 in bipropellant systems, in hybrid rockets, as a monopropellant, and as a secondary injection fluid. In addition, extensive data are given on the propellant's heat transfer characteristics, storability, radiation resistance, and materials compatibility. (Author)
The 98% H2O2 Monomethyl Hydrazine Propeliant Combination and Its Suitability for the Gemini Spacecraft Attitude Control System
1963
24 pages
Report
No indication
English
Temperature-entropy diagram of monomethyl- hydrazine
AIAA | 1964
|Gelled Monomethyl Hydrazine Hypergolic Droplet Investigation
Online Contents | 2013
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