MECHANISM OF CATALYTIC IGNITION AND COMBUSTION OF SOLID ROCKET PROPELLANTS (U).

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)

Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1967
Accession Number
AD0650447

Entities

People

  • L. Dauerman

Organizations

  • New York University

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Burning Rate
  • Combustion
  • Double Base Propellants
  • Ignition
  • Propellants
  • Rocket Propellants
  • Solid Rocket Propellants
  • Surface Temperature

Fields of Study

  • Physics

Readers

  • Rocket Propulsion.