The propellants are used as rocket propulsion fuels. They contain from 44 to 60 percent nitrocellulose, 28 to 47 percent nitroglycerin, from 2 to 5 percent of a ballistic modifier such as lead salicylate and a benzophenone such as 2,4-dihydroxybenzophenone.
Base Propellants of Increased Burning Rate Containing Benzophenones
1966
1 pages
Report
No indication
English
Unsteady Burning of Double-Base Propellants
AIAA | 1983
|Burning rate characteristics of GAP propellants
AIAA | 1990
|Burning rate characteristics of GAP propellants
AIAA | 1988
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