SECONDARY COMBUSTION OF PENTABORANE-HYDRAZINE EXHAUST IN AIR

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.

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1967
Accession Number
AD0819676

Entities

People

  • Robert C. Adrian
  • Robert E. Yates
  • Sanders D. Rosenberg

Organizations

  • Aerojet Rocketdyne Holdings

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Ceramic Materials
  • Chemical Reactions
  • Combustion
  • Combustion Chambers
  • Combustion Products
  • Combustors
  • Cooling
  • Fabrication
  • Heat Transfer
  • High Temperature
  • Hydrazines
  • Ignition
  • Light Sources
  • Materials
  • Measurement
  • Physical Properties

Fields of Study

  • Chemistry
  • Physics

Readers

  • Internal Combustion Engine (ICE) Technology.
  • Small Business Innovation Research Program (SBIR) EDI Research and Innovation.
  • Software Engineering