Accession Number : AD0819625
Title : COMBUSTION IRREGULARITIES OF SOLID PROPELLANTS.
Descriptive Note : Final summary rept. 1 Sep 63-30 Sep 65,
Corporate Author : UTAH UNIV SALT LAKE CITY DEPT OF CHEMICAL ENGINEERING
Personal Author(s) : Ryan, Norman W.
Report Date : 01 AUG 1967
Pagination or Media Count : 5
Abstract : Results are covered pertaining to attempts to increase the versatility of the standard T-burner, including variations in apparatus and technique of operation and new methods of treating the data obtained to extract information about pressure-coupled oscillatory combustion. In addition results are presented encompassing the research accomplished on solid propellant non-acoustic instability phenomena and on the developement of new type side-vented cylindrical burner utilizing premixed gaseous propellant. (Author)
Descriptors : *SOLID ROCKET PROPELLANTS), (*COMBUSTION, STABILITY, INSTRUMENTATION, OSCILLATION, SENSITIVITY, ACOUSTICS, BURNING RATE, HEAT TRANSFER, ROCKET PROPELLANT GRAINS, PRESSURE, CATALYSTS, ALUMINUM, AMMONIUM PERCHLORATE, VENTING, BUTADIENES, POLYMERS, SOLID ROCKET PROPELLANT BINDERS.
Subject Categories : Solid Rocket Propellants
Distribution Statement : APPROVED FOR PUBLIC RELEASE