FireDOC Search

displaying 1 - 10 results in total 79

  • Anderson, C. L.
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    Vulnerability Methodology and Protective Measures for Aircraft Fire and Explosion Hazards. Volume 3. On-Board Inert Gas Generator System (OBIGGS) Studies. Part 1. OBIGGS Ground Performance Tests. Final Report. August 1982 to July 1984.
    Boeing Military Airplane Co., Seattle, WA
    Aero Propulsion Lab., Wright-Patterson AFB, OH, AFWAL-TR-85-2060; D180-28862-1, January 1986, 187 p.

  • Grenich, A. F.
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    Vulnerability Methodology and Protective Measures for Aircraft Fire and Explosion Hazards. Volume 1. Executive Summary. Final Report. February 1981 to October 1984.
    Boeing Military Airplane Co., Seattle, WA
    Aero Propulsion Lab., Wright-Patterson AFB, OH, AFAW-TR-85-2060, January 1986, 39 p.

  • Hogan, T. A.; Pedriani, C.
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    Flame Tube and Ballistic Evaluation of Explosafe Aluminum Foil for Aircraft Fuel Tank Explosion Protection. Final Report. August 1977-March 979.
    Air Force Wright Aeronatucal Labs., Wright-Patterson AFB, OH
    AFWAL-TR-80-2031, March 1980, 98 p.

  • Kuchta, J. M.; Cato, R. J.; Martindill, G. H.; Spolan, I.
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    Ignition and Fire Suppression in Aerospace Vehicles. Technical Report. January 1, 1970-November 30, 1971.
    Bureau of Mines, Pittsburgh, PA
    Air Force Aero Propulsion Lab., Wright-Patterson AFB, OH, AFAPL-TR-71-93; PMSRC Report 4164, December 1971, 49 p.

  • Emmons, H. W.; Mitler, H. E.
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    Computer Modeling of Aircraft Cabin Fires. Final Report. June 1981-December 31, 1982.
    Harvard University, Cambridge, MA; Federal Aviation Administration, Washington, DC
    National Bureau of Standards, Gaithersburg, MD, NBS GCR 83-431; Home Fire Proj. Tech. Rpt. 57, June 1983, 93 p.

  • Roth, A. J.
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    Development and Evaluation of an Airplane Fuel Tank Ullage Composition Model. Volume 2. Experimental Determination of Airplane Fuel Tank Ullage Compositions. Final Report. November 1985-December 1986.
    Boeing Military Airplane Co., Seattle, WA
    Air Force Wright Aeronautical Labs., Wright-Patterson AFB, OH, AFWAL-TR-87-2060, October 1987, 116 p.

  • Geyer, G. B.; Urban, G. H.
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    Evaluation of an Improved Flame Resistant Aircraft Window System. Final Report.
    Federal Aviation Admin., Atlantic City Airport, NJ
    DOT/FAA/CT-83/10; ACT-350, May 1984, 61 p.

  • Desmarais, L. A.; Tolle, F. F.
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    Integrated Aircraft Fuel Tank Inerting and Compartment Fire Suppression System. Volume 1. Preliminary Design, Optimization, and Integration. Final Report. August 1979-October 1982.
    Boeing Military Airplane Co., Seattle, WA
    Aero Propulsion Lab., Wright-Patterson AFB, OH, AFAPL-TR-83-2021, Volume 1, April 1983, 107 p.

  • Johnson, R. L.; Gillerman, J. B.
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    Aircraft Fuel Tank Inerting System. Final Report. May 8, 1978-July 30, 1983.
    AiResearch Manufacturing Co., Torrance, CA
    Aero Propulsion Lab., Wright-Patterson AFB, OH, AFWAL-TR-82-2115, July 1983, 253 p.

  • Stein, A.; Regent, L. S.
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    Aircraft Fuel Tank/System Data Analysis. Volume 3. Variable Selection Report. Final Report. February 28, 1975-September 30, 1976.
    Falcon Research and Development Co., Denver, CO
    Air Force Flight Dynamics Lab., Wright-Patterson AFB, OH, AFFDL-TR-76-39-VOL-3; FR/D-BUF-4-VOL-3, November 1976, 38 p.