Accession Number : AD0630409

Title :   COMBUSTION IRREGULARITIES IN SOLID PROPELLANTS.

Descriptive Note : Final rept., Aug 62-Aug 63,

Corporate Author : UTAH UNIV SALT LAKE CITY DEPT OF CHEMICAL ENGINEERING

Personal Author(s) : Ryan,Norman W.

Report Date : 04 MAR 1966

Pagination or Media Count : 11

Abstract : In studies employing the side-vented end-burner, the participation of the solid phase in acoustic oscillations was quantitatively confirmed and described. In cooperation with other laboratories, the usefulness of the burner for propellant evaluation was demonstrated. Initial experiments in a study of non-acoustic instability were performed. (Author)

Descriptors :   (*SOLID ROCKET PROPELLANTS, COMBUSTION), (*COMBUSTION, ACOUSTICS), STABILITY, OSCILLATION, SOLIDS, TEST EQUIPMENT

Subject Categories : Combustion and Ignition
      Solid Rocket Propellants

Distribution Statement : APPROVED FOR PUBLIC RELEASE