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