INVESTIGATION OF FIRE EXTINGUISHING AGENTS FOR SUPERSONIC TRANSPORT

Abstract

Properties of ten compounds which have passed screening for possible use in the in-flight fire extinguishing system of the Supersonic Transport are tabulated. Reported are boiling points, freezing points, densities, viscosity- temperature relationships, vapor pressure-temperature curves, critical temperatures and pressures, heats of vaporization, specific heats pressures at 500 F and thermal stabilities under testing conditions. Also reported are the inhibitory effects of each compound on heptane-air flammabilities, estimated costs and compatibilities with various metallic and non metallic materials. Potential toxicities are discussed. Limited physical properties of an additional twenty-four materials which did not pass this preliminary screening are tabulated. Recommendations are given for more extensive work on acceptable compounds to further define their usefulness under Supersonic Transport flight conditions.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1963
Accession Number
AD0420822

Entities

People

  • Herbert Landesman
  • John E. Basinski

Tags

Communities of Interest

  • Counter IED
  • Ground and Sea Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Boiling Point
  • Chemical Synthesis
  • Chemistry
  • Chlorides
  • Combustion
  • Critical Temperature
  • Heat Capacity
  • Heat Energy
  • Heat Of Vaporization
  • Materials
  • Measurement
  • Physical Properties
  • Specific Heat
  • Supersonic Transport Aircraft
  • Thermal Stability
  • Vapor Pressure
  • Viscosity

Readers

  • Aerospace Test and Evaluation
  • Combustion science or combustion engineering.
  • Fire Suppression Systems Design.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow