Accession Number:
AD0647950
Title:
MECHANISM OF CATALYTIC IGNITION AND COMBUSTION OF SOLID ROCKET PROPELLANTS.
Descriptive Note:
Bimonthly rept. no. 2, 24 Aug-23 Oct 66,
Corporate Author:
NEW YORK UNIV N Y DEPT OF CHEMICAL ENGINEERING
Personal Author(s):
Report Date:
1966-10-23
Pagination or Media Count:
8.0
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:
Subject Categories:
- Combustion and Ignition
- Solid Rocket Propellants