02027cam a2200349Ia 4500011444012MiAaHDL20141009010000.0m d cr bn ---auauacr cnu||||||||050207s1970 dcua b f000 0 eng dsdr-uiuc6401909(OCoLC)57582419egmEGMOCLCQAD#UIUUNAS 1.14:D-6013NASA-TN-D-6013Voelkl, Hans R.Thermal decomposition and explosion of ammonium perchlorate and ammonium perchlorate propellant up to 50 kilobars (5.0 x 10⁹ N/m²)[electronic resource] /Hans R. Voelkl.Washington, D.C. :National Aeronautics and Space Administration :[For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151],1970.22 p. :ill. ;27 cm.NASA technical note ;D-6013Includes bibliographical references (p. 21-22).The rates of thermal decomposition of ammonium perchlorate and an ammonium perchlorate solid propellant at 15, 25, and 50 kilobars (1.5X10 , 2.5X10 , and 5.0XlO N/m ) pressure were studied in a cubic anvil press. The data were correlated by first order rate equations to obtain the temperature variation of the specific reaction rates and the apparent activation energies. Explosion limits of pure ammunium perchlorate are included to 30 kilobars (3. OXlO9 N/m2). Electrical resistance measurements of this salt at high pressure were also made.Mode of access: Internet.System requirements: Adobe Acrobat Reader.Mode of access: World Wide Web.Rockets (Aeronautics)Solid propellant rockets.Solid propellants.Ammonium perchlorate.Lewis Research Center.United States.National Aeronautics and Space Administration.01144401220101109143919.020141009010000.020141112165512.02025-11-22T19:15:56Z2025-11-22T18:50:03ZSDR-UIUCUNKNOWNloader.pl-003-020BKsdr-uiuc6401909uiugSDRUIUCuiug.30112106691378UIU6401909UIUUIUC20251122googleuiug.301121066913781970pdbibUS fed doc