Search Results - "Fedorychev, A. V."

Combustion Model for a Composite Solid Propellant with an Evaporating Coolant by Fedorychev, A. V., Milekhin, Yu. M.

“…This paper presents a combustion model for a solid propellant consisting of a matrix capable of self-sustained combustion and particles of a polydisperse…”
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Condensed Products of Combustion of Boron-Based Solid Propellants by Fedorychev, A. V., Milekhin, Yu. M., Rashkovskii, S. A.

“…Condensed combustion products of model propellants based on aluminum boride in the combustion chamber of the gas generator of a ducted rocket engine have been…”
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Modeling of Ignition and Combustion of Boron-Containing Solid Propellants by Arkhipov, V. A., Basalaev, S. A., Kuznetsov, V. T., Poryazov, V. A., Fedorychev, A. V.

“…This paper presents the results of an experimental study of the ignition and slagging characteristics for combustion of boron-containing solid propellants with…”
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Mechanism of Stabilization of the Combustion in the Duct of the Solid Fuel Grain of a Solid Fuel Ramjet by Rashkovskii, S. A., Milekhin, Yu. M., Fedorychev, A. V., Yakush, S. E.

“…The mechanism of stabilization of the combustion in the duct of the solid fuel grain of a solid fuel ramjet with a flame holder was analyzed for the first…”
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Effect of distributed injection of air into the afterburning chamber of a ram-rocket engine on the efficiency of combustion of boron particles by Rashkovskii, S. A., Milekhin, Yu. M., Fedorychev, A. V.

“…A mathematical model of combustion of boron particles in a ram-rocket engine is developed. The boron combustion efficiency for one-stage and two-stage…”
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Improving the completeness of combustion of boron particles in a solid-fuel ducted rocket owing to distributed air supply to the secondary combustor by Rashkovskii, S. A., Milekhin, Yu. M., Fedorychev, A. V.

“…A model of combustion of boron particles in ducted rocket using distributed air supply to the secondary combustor was developed for the first time. The…”
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Correlation of parameters in the burning rate law and its influence on intraballistic characteristics of a rocket motor by Rashkovskiy, S. A., Milekhin, Yu. M., Fedorychev, A. V.

“…Experimental data demonstrating the correlation of parameters in the power-law dependence of the burning rate of composite solid propellants on pressure are…”
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Two-zone model for combustion of a composite solid propellant with a coolant by Strunin, V. A., Fedorychev, A. V., Gunin, S. V., Klyuchnikov, A. N., Milekhin, Yu. M., Manelis, G. B.

“…A mathematical model for combustion of a propellant with a coolant taking into account the two-zone structure of the combustion front due to condensed- and…”
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Effect of tension of a composite propellant on its burning rate by Rashkovsky, S. A., Milyokhin, Yu. M., Klyuchnikov, A. N., Fedorychev, A. V.

“…Existing concepts of the effect of tensile strains on the burning rate of propellants are analyzed. It is demonstrated that the basic mechanism of increasing…”
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Solid-propellant gas generators with a gas flow rate stabilization system by Rashkovskii, S. A., Milekhin, Yu. M., Fedorychev, A. V.

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Combustion mechanism of mixtures of binders capable of self-sustained combustion with inert and active fillers by Rashkovskii, S. A., Milekhin, Yu. M., Klyuchnikov, A. N., Fedorychev, A. V.

“…A single mechanism for the combustion of mixtures of binders capable of self-sustained combustion with inert or active fillers is proposed. A mathematical…”
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Method of the model equation in the theory of unsteady combustion of a solid propellant by Rashkovskii, S. A., Milekhin, Yu. M., Klyuchnikov, A. N., Fedorychev, A. V.

“…A model equation for the unsteady burning rate of a solid propellant is proposed and justified. In the frequency range of interest for practice, the proposed…”
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Bifurcations of the flow characteristics of an adjustable supersonic nozzle by Rashkovskii, S. A., Milekhin, Yu. M., Kluchnikov, A. N., Fedorychev, A. V.

“…A ground-based experimental study of the flow characteristic of an adjustable highaltitude nozzle was performed. It is shown that the flow characteristic of…”
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Effect of thermal radiation on unsteady combustion of condensed energy-rich systems by Novozhilov, B. V., Milekhin, Yu. M., Klyuchnikov, A. N., Fedorychev, A. V.

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Stability of combustion in solid-propellant rocket motors with pressure stabilization system by Rashkovskii, S. A., Milekhin, Yu. M., Fedorychev, A. V., Assovskii, I. G.

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Mechanism and laws of combustion of composite solid propellants with a coolant by Strunin, V. A., Fedorychev, A. V., Gunin, S. V., Klyuchnikov, A. N., Milekhin, Yu. M., Manelis, G. B.

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