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