Accession Number : ADD002419

Title :   Rocket Propellant with Acrylate Binder and Difluoroamino Plasticizer.

Descriptive Note : Patent,

Corporate Author : DEPARTMENT OF THE NAVY WASHINGTON D C

Personal Author(s) : Childs,Lewis B , Jr ; Martin,James D

Report Date : 20 Jan 1976

Pagination or Media Count : 4

Abstract : 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) 1/2-5 weight percent curing agent.

Descriptors :   *Patents, *Liquid rocket propellants, Crosslinking(Chemistry), Attenuation, Combustion, Stability, Binders, Plasticizers, Acrylic acid, Acrylates, Copolymers, Oxidizers, Curing, Burning rate, Missile site radar

Subject Categories : Polymer Chemistry
      Combustion and Ignition
      Liquid Rocket Propellants

Distribution Statement : APPROVED FOR PUBLIC RELEASE