Rocket Propellant with Acrylate Binder and Difluoroamino Plasticizer.
DEPARTMENT OF THE NAVY WASHINGTON D C
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This patent discusses high energy, low radar attenuation propellant comprising of 1 25-55 weight percent of a binder which itself comprises from 2-25 weight percent of a copolymer of acrylic acid and a lower alkyl acrylate and 75-98 weight percent of an energetic difluoroamino group containing plasticizer, 2 0-15 weight percent aluminum or boron 3 45-75 weight percent of an oxidizer and 4 12-5 weight percent curing agent.
- Polymer Chemistry
- Combustion and Ignition
- Liquid Rocket Propellants