Accession Number:

AD0722084

Title:

Combustion Mechanism of Composite Propellants During Depressurization.

Descriptive Note:

Progress rept. no. 2, 1 Jul-31 Dec 70,

Corporate Author:

DEUTSCHE FORSCHUNGS- UND VERSUCHSANSTALT FUER LUFT- UND RAUMFAHRT E V TRAUEN (WEST GERMANY)

Personal Author(s):

Report Date:

1971-01-31

Pagination or Media Count:

30.0

Abstract:

Apparatus required to investigate the depressurization extinguishment behavior of solid propellants was constructed and a series of tests was conducted using a number of AP propellant compositions at several pressure levels. The results define more clearly the effects of these parameters on the dynamic behavior of the flame. A summary of the findings plus a detailed description of the apparatus and procedures used is given in the report. Author

Subject Categories:

  • Combustion and Ignition
  • Rocket Propellants

Distribution Statement:

APPROVED FOR PUBLIC RELEASE