Accession Number : AD0376429
Title : THE DEVELOPMENT AND EVALUATION OF A HYDROCARBON BINDER FOR HIGH ENERGY SOLID PROPELLANTS.
Descriptive Note : Quarterly rept. no. 2, 14 Jun-13 Sep 66,
Corporate Author : AEROJET-GENERAL CORP SACRAMENTO CALIF SOLID PROPELLANT OPERATIONS
Personal Author(s) : Johnson,Duane E. ; Di Milo,Anthony J.
Report Date : OCT 1966
Pagination or Media Count : 62
Abstract : Compatibility studies were extended to include epoxide and aziridine curing agents as well as isocyanates and the oxidizer hydroxylamine perchlorate. Hydroxy and olefinic functional groups are compatible with 'as received' LMH-1 and -2 and chrome coated Be, but carboxy groups were not. All these functional groups were compatible with hydroxylamine perchlorate. Isocyanate was the only curing agent which is practical in the hydroxylamine perchlorate system. (Author)
Descriptors : (*SOLID ROCKET PROPELLANT BINDERS, HYDROCARBONS), DENSITY, VISCOSITY, COMPATIBILITY, POLYMERS, SOLID ROCKET PROPELLANT PLASTICIZERS, BURNING RATE, AGING(MATERIALS), VOLUME, PARTICLE SIZE (U) ALUMINUM, BUTADIENES, AMMONIUM COMPOUNDS, PERCHLORATES, ISOCYANIC ACID
Subject Categories : Solid Rocket Propellants
Distribution Statement : APPROVED FOR PUBLIC RELEASE