INVESTIGATION OF PYROTECHNIC GENERATED GAS DISCHARGE FIRE EXTINGUISHING SYSTEM.

Abstract

Advanced aircraft operating in supersonic and hypersonic flight regimes will impose many environmental problems on aircraft subsystems. Fire extinguishing equipment will be required to operate efficiently over a -65F to 500F temperature range. To meet this requirement, a subscale Pyrotechnic Fire Extinguishing System was designed, developed and fire tested under simulated flight conditions. (Author)

Document Details

Document Type
Technical Report
Publication Date
May 01, 1968
Accession Number
AD0833991

Entities

People

  • L. V. Hebenstreit
  • M. Derouville

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircraft Equipment
  • Aircrafts
  • Extinguishing
  • Flight
  • Gas Discharges
  • Hypersonic Flight
  • Vehicle Equipment

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Fire Suppression Systems Design.
  • Systems Analysis and Design

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow