Accession Number : AD0648659
Title : MECHANISM OF CATALYTIC IGNITION AND COMBUSTION OF SOLID ROCKET PROPELLANTS.
Descriptive Note : Bimonthly rept. no. 1, 24 Jun-23 Aug 66,
Corporate Author : NEW YORK UNIV N Y DEPT OF CHEMICAL ENGINEERING
Personal Author(s) : Dauerman,L.
Report Date : 23 AUG 1966
Pagination or Media Count : 8
Abstract : The objective is to investigate the mechanism of action of burning rate catalysts in the ignition and combustion of double-base propellants. Experimentally, the surface temperatures of burning propellant strands are measured and chemical-kinetic investigations of the products of degradation of the regressing surface are carried out. Heat is supplied by an arc image furnace for the ignition studies. (Author)
Descriptors : (*SOLID ROCKET PROPELLANTS, COMBUSTION), DOUBLE BASE ROCKET PROPELLANTS, IGNITION, CATALYSIS, NITROGEN OXIDES, BURNING RATE, CATALYSTS, PYROLYSIS
Subject Categories : Combustion and Ignition
Solid Rocket Propellants
Distribution Statement : APPROVED FOR PUBLIC RELEASE