Patent, Filed 9 Nov 81, patented 12 Jul 83,
DEPARTMENT OF THE NAVY WASHINGTON DC
Pagination or Media Count:
A solid ramjet fuel composition comprising a hydroxyl terminated or carboxyl-terminated fluorocarbon binder, a polybutadiene prepolymer, a curative cross-linking compound, and a metal selected from the group consisting of aluminum, zirconium, amorphous boron or magnesium.
- Jet and Gas Turbine Engines
- Polymer Chemistry