Search
All articles by "Yagodnikov D.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 |
An Experimental Study of Electrophysical Characteristics of Gas Flow when Bench Testing Elements of Flow Ducts in Ramjets
| Authors: Rudinskiy A.V., Aleksandrov V.Yu., Yagodnikov D.A. | Published: 18.04.2017 |
| Published in issue: #4(685)/2017 | |
| Category: Technology and Process Machines | |
| Keywords: ramjet engine, fire tests, electrophysical diagnostics, gas flow magnetometer, magnetic field strength |
Special Features of Calculating the Composition and Temperature of Combustion Products of Superrich Oxygen-Methane Fuel
| Authors: Dorofeev A.A., Yagodnikov D.A., Chertkov K.O. | Published: 29.10.2015 |
| Published in issue: #10(667)/2015 | |
| Category: Aviation, Rocket and Technology | |
| Keywords: superrich oxygen-methane fuel, soot formation, chemical non-equilibrium, thermodynamic calculation, liquid propellant rocket engine, liquid gas generator |
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 |