Accession Number:

AD0802189

Title:

RESPONSE OF A BURNING PROPELLANT SURFACE TO EROSIVE TRANSIENTS

Descriptive Note:

Quarterly rept. no. 3, 1 Jul-30 Sep 1966

Corporate Author:

STANFORD RESEARCH INST MENLO PARK CA

Report Date:

1966-10-12

Pagination or Media Count:

26.0

Abstract:

Theoretical analysis of the unstable behavior of solid propellants has permitted the propellant response preferred frequencies to be calculated in terms of burning rate and activation energies for solid and gas phase reactions. The fractional heat release in the condensed phase reactions has been shown to be of importance in determining the magnitude of the propellant response.

Subject Categories:

  • Solid Rocket Propellants

Distribution Statement:

APPROVED FOR PUBLIC RELEASE