VULNERABILITY METHODOLOGY AND PROTCTIVE MEASURES FOR AIRCRAFT FIRE AND EXPLOSION HAZARDS

No abstract provided.

  • Supplemental Notes:
    • BOEING MILITARY AIRPLANE COMPANY OTHER PHYS. DESCRIPTION: 6 V ILLUSTRATED AUTHORS: A.F. GRENICH, A.M. JOHNSON, L.A. DESMARAIS, C.L. ANDERSON, P.M. MCCONNELL, G.A. DALAN JANUARY 1986 CONTENTS: V. I. EXECUTIVE SUMMARY -- V. II. AIRCRAFT ENGINE NACELLE FIRE TEST PROGRAM: PT. 1. FIRE DETECTION, FIRE EXTINGUISHMENT AND HOT SURFACE IGNITION STUDIES -- PT. 2. SMALL SCALE TESTING OF DRY- CONTENTS: AL FIRE EXTINGUISHANTS -- V. III. ON-BOARD INERT GAS GENERATOR SYSTEM OBIGGS STUDIES: PT. 1. OBIGGS GROUND PERFORMANCE TESTS -- PT. 2. FUEL SCRUBBING AND OXYGEN EVOLUTION TESTS -- PT. 3. A- CONTENTS: IGGS DESIGNS ADDL CORP. AUTHOR INFO: BOEING MILITARY AIRPLANE COMPANY ADDL CORP. AUTHOR INFO: AIR FORCE AERO PROPULSION LABORATORY U.S AERO PROPULSION LABORATORY AIR FORCE WRIGHT AERONAUTICAL LABORATORIES
  • Corporate Authors:

    AERO PROPULSION LABORATORY AIR FORCE SYSTEMS

    WRIGHT-PATTERSON AFB, OH  United States 
  • Authors:
    • GRENICH, A F
    • Johnson, A M
    • DESMARAIS, L A
    • Anderson, C L
  • Publication Date: 1986-1

Language

  • English

Subject/Index Terms

Filing Info

  • Accession Number: 00415701
  • Record Type: Publication
  • Source Agency: UC Berkeley Transportation Library
  • Report/Paper Numbers: AFWAL-TR-85-2060 FINAL REPO
  • Files: TLIB
  • Created Date: Oct 31 1986 12:00AM