CPC C06B 31/28 (2013.01) [C06B 23/001 (2013.01); C06B 23/006 (2013.01); C06C 9/00 (2013.01); C06D 5/10 (2013.01); F02K 9/24 (2013.01); F02K 9/26 (2013.01); F02K 9/425 (2013.01); F02K 9/70 (2013.01); F02K 9/72 (2013.01)] | 11 Claims |
1. A fuel that can be used for a rocket motor comprising:
a. an oxidizer containing greater than 10 wt. % water and an ionic liquid, said ionic liquid having a density of greater than 1.3 g/cc;
b. a fuel grain fabricated from a polymeric material with a density of at least 1.25 g/cc, said fuel grain contains about 10-50% metal fuel additions, said metal fuel additions including one or more metals selected from the group consisting of aluminum, aluminum-magnesium, magnesium, TiH2, AlMgB14, CaB6, AlB2, MgB2, SiB6, and boron.
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