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All articles by "Vorozheeva O.A."
Modeling and Calculating the Probability of Failure-Free Operation of a Liquid Low-Thrust Rocket Engine by Temperature Margin
| Authors: Vorozheeva O.A., Yagodnikov D.A., Ageenko Y.I. | Published: 06.09.2018 |
| Published in issue: #8(701)/2018 | |
| Category: Aviation, Rocket and Technology | Chapter: Aerodynamics and Heat Transfer Processes in Aircraft | |
| Keywords: probability of failure-free operation, liquid rocket engine, low-thrust engine, nitrogen tetroxide, unsymmetrical dimethylhydrazine, pulse mode |
Numerical Analysis of the Thermal State of the Resonator in a Gas-Dynamic Ignition System with Two-Phase Fuel Composition
| Authors: Vorozheeva O.A., Arefyev K.Yu. | Published: 11.05.2016 |
| Published in issue: #5(674)/2016 | |
| Category: Aviation, Rocket and Technology | |
| Keywords: thermal state, gas-dynamic ignition system, two-phase fuel composition, mathematical modeling, ethanol, temperature field, resonator, pulsed mode |
Study of the thermal state of a resonator in a gas-dynamic system initiating monopropellant decomposition
| Authors: Vorozheeva O.A., Arefyev K.Yu. | Published: 04.07.2014 |
| Published in issue: #7(652)/2014 | |
| Category: Calculation and Design of Machinery | |
| Keywords: gas-dynamic system, thermal state, monopropellant, mathematical modeling |
Mathematical Model and Computational Research of Combustion Chamber Wall Thermal State for Gaseous-Propellant Oxygen-Methane Low-Thrust Rocket Engine on a Pulse Mode
| Authors: Vorozheeva O.A., Yagodnikov D.A. | Published: 19.09.2013 |
| Published in issue: #7(640)/2013 | |
| Category: Calculation and Design of Machinery | |
| Keywords: low-thrust rocket engine, gaseous oxygen and methane, combust ion chamber, mathematical modeling, pulse mode, thermal state |