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27 search results for "propulsion system"
3.1.2020 Analysis of the unsteady stress-strain behavior of the launch vehicle hold-down bay at liftoff
Firstly, the unsteady heat fields on the hold-down bay surface are calculated by means of the semi-empirical method, which is based on the simulated results of the combustion [...]
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17.1.2020 Acoustic problems of rocket launch
Acoustic loads generated by the propulsion system.
12.1.2020 Modification of technology as the main course in the military transport aircraft development
Along with the traditional methods of designing the modifications, the domestic school proposed a new methodology for determining the necessary parameters for “deep” modifications [...]
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18.2.2018 Angular Stabilization of an Object Rapidly Rotating around Longitudial Axis
Spinning significantly increases stability of a moving object and partially evens out the negative impact of external and internal disturbing factors (skewness and eccentricities of [...]
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17.2.2018 Peculiarities of Dynamics of Recoverable Part of Stage of Aircraft-Type Configuration with Turbojet Engine
This recovery plan differs from an alternative rocket recovery system and, from our point of view, provides more efficient usage of the fuel stores because it doesn’t require [...]
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12.2.2018 Methodological Support for Initial Phase Optimization of Projecting Design, Trajectory Parameters and Rocket Object Motion Control Programs
Flight Control Optimization and Thrust Optimization of Controllable Rocket Object Main Propulsion System.
5.2.2018 Electromagnetic Valves Developed by Yuzhnoye SDO Liquid Rocket Engines Design Office
2018 (2); 34-48 DOI: https://doi.org/10.33136/stma2018.02.034 Language: Russian Annotation: In the pneumohydraulic systems of liquid rocket engines and propulsion [...]
Read more 5.2.2018 Electromagnetic Valves Developed by Yuzhnoye SDO Liquid Rocket Engines Design Office
3.2.2018 Possible Ways of Modernization of VEGA Launch Vehicle AVUM Stage Main Engine Assembly
Enhancing the capabilities of payload injection by launch vehicles into various orbits of artificial Earth satellites is the main task for the developers of ILV as a whole and for [...]
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2.2.2018 Yuzhnoye SDO-Developed Upper Stage Liquid Rocket Engines
In this case, RD809M engine is RD8 version with tight integration and RD809K engine is its one-chamber version; RD805 engine operating on liquid oxygen + kerosene created on the [...]
Read more 2.2.2018 Yuzhnoye SDO-Developed Upper Stage Liquid Rocket Engines
1.2.2018 Design Office of Liquid Rocket Engines is 60
At present, Yuzhnoye SDO jointly with SE PA Yuzhny Machine-Building Plant deliver the engine for the European Vega LV forth stage propulsion system under the contract [...]
Read more 1.2.2018 Design Office of Liquid Rocket Engines is 60