FireDOC Search

displaying 1 - 10 results in total 14

  • Olson, L. H.
    view article (1.0)

    Fire Detection and Extinguishing Subsystem Specification. Supersonic Transport Development Program. Phase 3 Proposal. Boeing Model 2707.
    Boeing Co., Seattle, WA
    D6A10115-1
    Federal Aviation Agency, Washington, DC, D6A10115-1
    September 7, 1966
    35 p.

  • Eggleston, L. A.; Hoffman, H. I.; Smith, H. M.; Yuill, C. H.
    view article (1.0)

    Feasibility Study of a Crash-Fire Prevention System for the Supersonic Commercial Transport. Technical Documentary Report.
    Southwest Research Inst., San Antonio, TX
    ASD-TDR-63-478
    Federal Aviation Agency, Washington, DC, ASD-TDR-63-478
    August 1, 1963
    111 p.

  • Skembare, H.; Springer, R. J.
    view article (1.0)

    Explosion/Fire Protection for Compartments Susceptible to Leakage of Combustibles on Advanced Aerospace Vehicles.
    General Dynamics, Fort Worth, TX
    ['ERR-FW-1203', 'RDP Task 414-14-594']
    ERR-FW-1203; RDP Task 414-14-594
    December 31, 1971
    91 p.

  • Helgeson, N. L.; Gerstein, M.; Breen, B. P.
    view article (1.0)

    Supersonic Aircraft Fuel Tank Fire Hazard Investigation. Technical Report.
    Air Force Aero Propulsion Lab., Wright-Patterson AFB, OH
    AFAPL-TR-68-106
    AFAPL-TR-68-106
    December 1968
    98 p.

  • Durkee, E. D.
    view article (1.0)

    Structural Temperatures at Supersonic Flight From B-58A and F-105D Aircraft. Technical Report.
    Air Force Flight Dynamics Lab., Wright-Patterson AFB, OH
    AFFDL-TR-65-162
    AFFDL-TR-65-162
    November 1965
    61 p.

  • Madgwick, T.
    view article (1.0)

    Look at Aircraft Fire Precautions and Protection.
    British Aircraft Corp., Weybridge
    Aircraft Engineering, Vol. 30, 29-31, February 1967

  • Miller, R. E.
    view article (1.0)

    Fuel Safety in Supersonic Flight.
    RAE, Farnborough, England
    Flight International, 338-339, March 4, 1965

  • Hill, R.
    view article (1.0)

    Feasibility of Detecting a Burner-Can Burn-Through by Means ofCO, CO2, Pressure, and Air Temperature Levels in a Jet Engine Nacelle. Final Report. January 1972-July 1973.
    Federal Aviation Administration, Atlantic City, NJ
    FAA-RD-74-18
    Federal Aviation Administration, Washington, DC, FAA-RD-74-18
    March 1974
    25 p.

  • Mead, C. F.; Spoecker, W. W.; Hoben, H. E.
    view article (1.0)

    Summary of Autoignition Tests.
    Lockheed Aircraft Co., CA
    LR 18475
    LR 18475
    January 8, 1965
    189 p.

  • Gerstein, M.; Allen, R. D.
    view article (1.0)

    Fire Protection Research Program for Supersonic Transport. Technical Documentary Report.
    Air Force Aero Propulsion Lab., Wright-Patterson AFB, OH
    ['APL TDR-64-105', 'Project 648D']
    Dynamic Science Corp., South Pasadena, CA, APL TDR-64-105; Project 648D
    October 1964
    231 p.