Accession Number:

AD0823199

Title:

SECONDARY COMBUSTION OF PENTABORANE-HYDRAZINE EXHAUST IN AIR.

Descriptive Note:

Quarterly progress rept. 1 Aug-31 Oct 67,

Corporate Author:

AEROJET-GENERAL CORP SACRAMENTO CA

Report Date:

1967-11-01

Pagination or Media Count:

36.0

Abstract:

The installation of the first of two liquid micromotors is nearing completion. These facilities will be used for the determination of the characteristic velocity and chamber temperature and for analysis of the exhaust products. Installation of the combustor, air-heater and exhaust sampling equipment is under way. The spectral equipment has been assembled and will be installed as required. The experimental study of the combustion characteristics in air of the exhaust products of the pentaborane-hydrazine system will be initiated when the installation of the facilities has been completed. Author

Subject Categories:

  • Test Facilities, Equipment and Methods
  • Combustion and Ignition
  • Liquid Propellant Rocket Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE