Accession Number : AD0829888

Title :   PARAMETRIC STUDY OF ROCKET INSTABILITY.

Descriptive Note : Final rept.,

Corporate Author : PURDUE UNIV LAFAYETTE IN SCHOOL OF MECHANICAL ENGINEERING

Personal Author(s) : Osborn, J. R. ; Netzer, D. W.

Report Date : 15 FEB 1968

Pagination or Media Count : 8

Abstract : The research program was concerned with (1) the problem of high frequency longitudinal pressure oscillations in premixed gaseous propellant combustors and (2) the steady-state and stability operating characteristics of bi-phase propellant rocket combustors operating at sub-critical conditions. Both analytical and experimental work were performed in order to study the aforementioned problems. (Author)

Descriptors :   (*ROCKET ENGINES, COMBUSTION), COMBUSTION CHAMBERS, GASEOUS ROCKET PROPELLANTS, BIPROPELLANTS, STABILITY, OSCILLATION, PRESSURE, VAPORIZATION.

Subject Categories : Combustion and Ignition
      Liquid Propellant Rocket Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE