Accession Number:

AD0819676

Title:

SECONDARY COMBUSTION OF PENTABORANE-HYDRAZINE EXHAUST IN AIR

Descriptive Note:

Quarterly progress rept. 1 May-31 Jul 1967

Corporate Author:

AEROJET-GENERAL CORP SACRAMENTO CA

Report Date:

1967-08-01

Pagination or Media Count:

61.0

Abstract:

The design of the first of two liquid micromotors, has been completed. This micromotor will be used for the determination of characteristic velocity, chamber temperature and analysis of the exhaust products. The preparation of the test sight has begun and the fabrication and installation of the micromotor and auxiliary equipment has been initiated. A tentative test plan has been developed for the study of the combustion characteristics in air of the pentaborane-hydrazine system.

Subject Categories:

  • Rockets
  • Combustion and Ignition

Distribution Statement:

APPROVED FOR PUBLIC RELEASE