Accession Number:

AD0272062

Title:

TWO-DIMENSIONAL MOTOR PROGRAM

Descriptive Note:

Interim rept. Dec 1960-Dec 1961

Corporate Author:

AEROJET-GENERAL CORP AZUSA CA

Report Date:

1962-01-01

Pagination or Media Count:

78.0

Abstract:

A two-dimensional motor was designed, fabricated, and tested to establish improved techniques for measuring the dynamic characteristics of the combustion mechanism in an operating thrust chamber. The criteria on which the design of the motor was based, the experimental equipment,AND THE TESTS CONDUCTED ARE DESCRIBED. The methods by which this motor can be used to investigate stable and unstable combustion are discussed and the correlations necessary to relate the observed phenomena to the behavior of full-scale rocket engines are indicated.

Subject Categories:

  • Combustion and Ignition

Distribution Statement:

APPROVED FOR PUBLIC RELEASE