Fire Suppression for Aerospace Vehicles

Abstract

Fire extinguishing experiments were conducted to evaluate Halon 1301 (bromo-trifluoromethane) as an extinguishant of Class A fires by the total flooding mode for possible use in advanced aircraft. The effectiveness of the extinguishant was determined by burning cotton sheeting fires in a 216 cu ft chamber at various combustible loadings, preburn times, and extinguishant discharge pressures or rates. A 3 percent Halon concentration appeared to be inadequate under most test conditions. With 6 percent Halon, the toxicity hazard from the formation of CO, HF, or HBr was relatively small for preburn times of 15 seconds or less. The concentration of toxic product vapors increased noticeably when the total burning period before extinguishants was increased from 15 to 25 seconds. Under all test conditions, the toxic product concentrations reported for short exposure times. Data are also presented on the rates of pressure rise and mass consumption that characterized the cotton sheeting fires.

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1970
Accession Number
AD0874046

Entities

People

  • George H. Martindill
  • Irving Spolan
  • Joseph M. Kuchta

Tags

Communities of Interest

  • Air Platforms
  • Space

DTIC Thesaurus Topics

  • Aerospace Craft
  • Air Force
  • Aircrafts
  • Boiling Point
  • Combustion
  • Combustion Products
  • Decomposition
  • Fire Extinguishers
  • Fire Extinguishing Agents
  • Fire Protection
  • Fire Suppression
  • Fires
  • Floods
  • Gases
  • Physical Properties
  • Standards
  • Vehicles

Readers

  • Fire Suppression Systems Design.
  • Mathematics or Statistics

Technology Areas

  • Space
  • Space - Hall-Effect Thruster