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) : Steinz,J. A. ; Selzer,H.
Report Date : 31 JAN 1971
Pagination or Media Count : 30
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)
Descriptors : (*COMPOSITE PROPELLANTS, *COMBUSTION), SOLID ROCKET PROPELLANTS, AMMONIUM PERCHLORATE, STABILITY, TEST EQUIPMENT, COMBUSTION CHAMBERS, PRESSURIZATION, WEST GERMANY
Subject Categories : Combustion and Ignition
Distribution Statement : APPROVED FOR PUBLIC RELEASE