Propellant Composition with a Nitro Containing Cross-Linked Binder.
DEPARTMENT OF THE NAVY WASHINGTON D C
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The patent describes a high energy propellant composition comprising a binder, oxidant, fuel and plasticizer. An energetic binder for said composition is prepared by reacting a nitro or fluorodinitromethyl containing polycarboxylic acid-diol type polyester with an isocyanate or a carboxyl reactive crosslinking agent.
- Solid Rocket Propellants