displaying 31 - 40 results in total 138
Miller, M. S.; Holmes, H. E.
view article (1.0)Experimental Determination of Subatmospheric Burning Rates and Critical Diameters for AP/HTPB Propellant. Final Report. November 1986-September 1987.Army Ballistic Research Lab., Aberdeen Proving Ground, MDBRL-MR-3719, December 1988, 26 p.Schroeder, M. A.
view article (1.0)Thermal Decomposition of RDX and RDX-Borohydride Mixtures. Final Report. January 1986-December 1986.Army Ballistic Research Lab., Aberdeen Proving Ground, MDBRL-MR-3699, September 1988, 48 p.Mason, C. M.; Gibson, F. C.; Summers, C. R.; Scott, F. H.
view article (1.0)Studies on Deflagration to Detonation in Propellants and Explosives. Quarterly Report. July 1, 1959-September 30, 1959.Bureau of Mines, Pittsburgh, PAARPA Order 44-59, December 4, 1959, 13 p.McGill, R.
view article (1.0)Explosives, Propellants and Pyrotechnic Safety Covering Laboratory, Pilot Plant, and Production Operations.Naval Ordnance Lab., Silver Spring, MDNOLTR 61-138, February 1962, 98 p.Roberts, D. J.
view article (1.0)Aerosols and Fire Prevention.British Aerosol Manufacturers' Association (BAMA)Fire Prevention, No. 217, 24-27, March 1989Saito, T.; Maruyama, T.; Higashi, K.; Iwama, A.
view article (1.0)Ignition of Laminated Composite Propellants Composed of Ammonium Perchlorate Single Crystal and Fuel-Binder Slab by Means of CO2 Laser. Short Communication.Tokyo Univ., JapanCombustion Science and Technology, Vol. 15, 161-168, 1976Price, D.; Clairmont, A. R., Jr.
view article (1.0)Explosive Behavior of Simplified Propellant Models.Naval Surface Weapons Center, Silver Spring, MDCombustion and Flame, Vol. 29, 87-93, 1977Girdhar, H. L.; Arora, A. J.
view article (1.0)Effect of Pressure on Heat of Explosion.Kashmir Univ., Srinagar, IndiaCombustion and Flame, Vol. 28, No. 3, 291-293, 1977Suhas, H. K.; Bose, T. K.
view article (1.0)Mathematical Model to Predict Transient Burning Rate and Pressure Decay Rates for Extinction of Composite Propellants.Indian Institute of Technology, Madras, IndiaCombustion and Flame, Vol. 28, No. 2, 145-153, 1977Niioka, T.; Mitani, T.; Ishii, S.
view article (1.0)Transient Period of the Acceleration-Produced Burning Rate Augmentation.National Aerospace Lab., Miyagi, JapanAIAA Journal, Vol. 14, No. 9, 1165-1169, September 1976