Effect of application of various ignition conditions in closed-vessel tests on burning rate calculation of a fine-grained propellant

By Leciejewski Zbigniew  

Combustion, Explosion, and Shock Waves, Vol. 47, Iss. 2, 2011-03 ,pp. : 209-216

Springer Publishing Company

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Burning-rate behavior in aluminized wide-distribution AP composite propellants

By Brewster M.  

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Effect of the addition of ultrafine aluminum powders on the rheological properties and burning rate of energetic condensed systems

By Popenko E.   Gromov A.   Shamina Yu.   Il’in A.   Sergienko A.   Popok N.  

Combustion, Explosion, and Shock Waves, Vol. 43, Iss. 1, 2007-01 ,pp. : 46-50

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Two-zone model for combustion of a composite solid propellant with a coolant

By Strunin V.   Fedorychev A.   Gunin S.   Klyuchnikov A.   Milekhin Yu.   Manelis G.  

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Laser technique for determining solid propellant transient burning rates during oscillatory combustion

By Togel M.   Wiche G.   Propst F.   Junye W.   Bingcheng S.  

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