Solid hypergolic propellant systems
Abstract
Abstract Hypergolic solid oxidizer and fuel systems are provided whereby ignition and combustion of the separate solid fuel and oxidizer grains can be obtained by contacting of the respective grains. Suitable solid oxidizers include NOBrF4, LiClO4 . NOF, MgClO4 . 2NOF, NO2ClO4, NO2BF4, (NO2)3 (AlClO4)6, NO2AsF6, NO2SbF6, and NO2PF6. Suitable solid fuels include LiAlH4, LiBH4, Li2AlH5, BeH2, LiH2 . BeH2, tetramethylammonium hydrotriborate, triaminoguonidinium diazine, diaminotetrazine, 4-amino-3, 5dihydrazine-1,2,4-triazole, N2H4(BH3)2, Mu (hydrazino)decaborane, 3,6-dihydrazine-s-tetrazine, NH4N3, (CH3)4NB3H8 and borane complexes with ammonia such as B10H12 . 2NH3. Completely fluorinated polyethylene resin is a suitable binder for the oxidizer system.
Inventors
- 👤 B Iwanciow
- 👤 W Lawrence
Bibliographic Details
Claims Analysis
Total Claims: 7References Cited (Backward Citations)
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