Accession Number : ADA299478
Title : Combustion Mechanisms of Very High Burn Rate (VHBR) Propellant. Phase II.
Descriptive Note : Final rept. Jul 88-Jul 90,
Corporate Author : VERITAY TECHNOLOGY INC EAST AMHERST NY
Personal Author(s) : Barnes, James T. ; Fisher, Edward B.
PDF Url : ADA299478
Report Date : SEP 1995
Pagination or Media Count : 125
Abstract : In this Phase II Small Business Initiated Research (SBIR) program, the various combustion mechanisms of very high burn rate (VHBR) propellant formulations were studied. Toward this end, various diagnostic and specialized instrumentation techniques were developed and evaluated. These techniques included miniature strain gage instrumentation and cine x-ray experimentation. The program resulted in hypotheses regarding combustion mechanisms at work in VHBR propellant formulations.
Descriptors : *BURNING RATE, *SOLID ROCKET PROPELLANTS, HIGH RATE, COMBUSTION, STRAIN GAGES, INSTRUMENTATION, FORMULATIONS(CHEMISTRY).
Subject Categories : Combustion and Ignition
Solid Rocket Propellants
Distribution Statement : APPROVED FOR PUBLIC RELEASE