MECHANISM OF CATALYTIC IGNITION AND COMBUSTION OF SOLID ROCKET PROPELLANTS.
Bimonthly rept. no. 2, 24 Aug-23 Oct 66,
NEW YORK UNIV N Y DEPT OF CHEMICAL ENGINEERING
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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
- Combustion and Ignition
- Solid Rocket Propellants