All articles by "Borovik I.N."
Numerical Simulation of Kerosene Dispersion Process by the Centrifugal Atomizer
Authors: Strokach Е.А., Borovik I.N. | Published: 12.06.2016 |
Published in issue: #3(108)/2016 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
Keywords: numerical simulation, Sauter mean diameter, turbulence model, sheet constant, ligament constant, atomization, rocket engine |
Experimental Study of Performance of a 500-N Liquid-Propellant Rocket Engine using Kerosene and High-Concentration Hydrogen Peroxide
Authors: Chudina Yu.S., Borovik I.N., Kozlov A.A., Bogacheva D.Yu., Vorob’ev A.G., Zarankevich I.A., Tashev V.P., Kazennov I.S. | Published: 15.09.2014 |
Published in issue: #4(97)/2014 | |
DOI: | |
Category: Power-generating and Transport Machine Building | |
Keywords: low-thrust liquid-propellant rocket engine, hydrogen peroxide, kerosene, injector, catalytic package, regime parameters, ignition |
Evaluating the Probability of End-of-Life Failure-Free Performance of Liquid-Propellant Rocket Engine of Reusable Space Tug
Authors: Borovik I.N. | Published: 07.04.2014 |
Published in issue: #2(95)/2014 | |
DOI: | |
Category: Inspection and Diagnostics | |
Keywords: rocket engine, orbital transfer vehicle |
Research into thermal efficiency of film cooling along combustion chamber wall of low-thrust rocket engine
Authors: Kozlov A.A., Bogacheva D.Yu., Borovik I.N. | Published: 06.02.2014 |
Published in issue: #1(94)/2014 | |
DOI: | |
Category: Power-generating and Transport Machine Building | |
Keywords: low-thrust rocket engines, thermal efficiency of film cooling, chamber wall temperature |