FireDOC Search

displaying 31 - 40 results in total 111

  • Gilbert, J. W.; White, J. D.; Wierenga, P. H.
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    Fire Suppression Using Solid Propellant Gas Generator Technology.
    Primex Aerospace Co.
    Halon Options Technical Working Conference. Proceedings. HOTWC 1997. Sponsored by: University of New Mexico, Halon Alternative Research Corp., National Association of Fire Equipment Distributors, Inc., Hughes Associates, Inc., and Kidde International. May 6-8, 1997, Albuquerque, NM, 485-497 p., 1997

  • Wang, X.; Jackson, T. L.
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    Numerical Simulation of Two-Dimensional Aluminized Composite Solid Propellent Combustion.
    University of Illinois, Urbana-Champaign
    Combustion Theory and Modelling, Vol. 9, No. 1, 171-197, February 2005

  • Combustion Institute
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    Combustion Institute, Symposium (International) on Combustion, 30th. Proceedings. Volume 30. Part 2. July 25-30, 2004.
    Combustion Institute, Pittsburgh, PA
    Combustion Institute, Symposium (International) on Combustion, 30th. Proceedings. Volume 30. Part 2. July 25-30, 2004, Combustion Institute, Pittsburgh, PA, Chicago, IL, Chen, J. H.; Colket, M. D.; Barlow, R. S.; Yetter, R. A., Editors, 1705-3406 p., 2005

  • Sampson, W. P.
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    Development of a 100% Solid Propellant Based Gas Generator Fire Suppression System.
    ATK Launch Systems, Brigham City, UT
    HOTWC 2006,
    Halon Options Technical Working Conference, 16th Proceedings. HOTWC 2006. May 16-18, 2006, Albuquerque, NM, 1-11 p., 2006

  • Telengator, A. M.; Williams, F. A.; Margolis, S. B.
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    Finite-Rate Interphase Heat-Transfer Effects on Multiphase Burning in Confined Porous Propellants.
    University of California, San Diego, La Jolla; Sandia National Laboratories, Livermore, CA
    Combustion Science and Technology, Vol. 178, No. 9, 1685-1720, September 2006
    Combustion Process International Symposium, XVIII (18th). Proceedings. SELECTED PAPERS. September 2-5, 2003, Ustron, Poland, 2006

  • Giovangigli, V.; Meynet, N.; Smooke, M.
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    Application of Continuation Techniques to Ammonium Perchlorate Plane Flames.
    CMAP-CNRS, École Polytechnique, 91128 Palaiseau cedex, France; ONERA, 91128 Palaiseau, France; Yale Univ., New Haven, CT
    Combustion Theory and Modelling, Vol. 10, No. 5, 771-798, October 2006

  • Fennell, P. S.; Dennis, J. S.; Hayhurst, A. N.
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    Sampling of Nanoparticles of MgO Formed When Doping an Oxygen-Rich Flame With Magnesium: The Measurement of the Concentrations and Size-Distributions of These Nanoparticles.
    Cambridge Univ., England
    Combustion and Flame, Vol. 151, No. 4, 560-572, December 2007

  • Zhai, J.; Yang, R.; Li, J.
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    Catalytic Thermal Decomposition and Combustion of Composite BAMO-THF Propellants.
    Beijing Institute of Technology, Beijing 100081, People's Republic of China
    Combustion and Flame, Vol. 154, No. 3, 473-477, August 2008

  • Massa, L.
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    Spatial Linear Analysis of the Flow in a Solid Rocket Motor With Burning Walls.
    Texas Univ., Arlington
    Combustion and Flame, Vol. 156, No. 4, 865-888, April 2009

  • Kooker, D. E.; Anderson, R. D.
    view article (7.5512667)

    Modeling of Hivelite Solid Propellant.
    Army Ballistic Research Lab., Aberdeen Proving Ground, MD
    BRL-TR-2649, April 1985, 71 p.