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29 search results for "thrust"
2.1.2024 New and advanced liquid rocket engines of the Yuzhnoye SDO
Significant steps in this area have been made by the experts from the Yuzhnoye propulsion division and then subsequent manufacture and delivery by Yuzhmash PA of the engine intended [...]
Read more 2.1.2024 New and advanced liquid rocket engines of the Yuzhnoye SDO
3.1.2020 Analysis of the unsteady stress-strain behavior of the launch vehicle hold-down bay at liftoff
Inverse heat transfer method applied to capacitively cooled rocket thrust chambers. Thermal-structural analysis of regeneratively cooled thrust chamber wall in [...]
Read more 3.1.2020 Analysis of the unsteady stress-strain behavior of the launch vehicle hold-down bay at liftoff
17.1.2020 Acoustic problems of rocket launch
While saving the general thrust of the engine this method can not greatly reduce the sound radiation by a jet.
12.2.2018 Methodological Support for Initial Phase Optimization of Projecting Design, Trajectory Parameters and Rocket Object Motion Control Programs
The mathematical model of the guided missile provides adequate accuracy for design study to determine: overall dimensions and mass characteristics of the guided missile in general [...]
Read more 12.2.2018 Methodological Support for Initial Phase Optimization of Projecting Design, Trajectory Parameters and Rocket Object Motion Control Programs
10.2.2018 Calculation of Gas Flow in High-Altitude Engine Nozzle and Experience of Using Water-Cooled Nozzle Head during Tests
Thrust-Vectoring Nozzle Performance Mode-ling.
5.2.2018 Electromagnetic Valves Developed by Yuzhnoye SDO Liquid Rocket Engines Design Office
The present-day spacecraft gas-jet orientation and stabilization systems use as propulsion devices the electromagnetic valves with nozzles whose thrust is, as a rule, not [...]
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
2018 (2); 16-24 DOI: https://doi.org/10.33136/stma2018.02.016 Language: Russian Annotation: The Ukrainian companies Yuzhnoye SDO and SE PA YMZ supply VG143 main engine assembly for [...]
Read more 3.2.2018 Possible Ways of Modernization of VEGA Launch Vehicle AVUM Stage Main Engine Assembly
1.2.2018 Design Office of Liquid Rocket Engines is 60
Among them we should mention the RD858 and RD859 engines for the soviet lunar take-off-and –landing module of Block E, the unique RD857 and RD862 engines with afterburning of [...]
Read more 1.2.2018 Design Office of Liquid Rocket Engines is 60
7.2.2017 Features of Pneumatic Hydraulic Feeding System with the Use of Oxygen-Methane Cryogenic Propellants
Development of “Chase-10” liquid rocket engine having 10tf thrust using LOX & LNG (Methane).
2.1.2019 Flying Vehicle Maneuvering Dynamics in Atmosphere with Weight Asymmetry and Elements of Terminal Control in Turn Leg
2019, (1); 4-14 DOI: https://doi.org/10.33136/stma2019.01.004 Language: Russian Annotation: This paper suggests method for analysis of the dynamics of the aircraft with weight [...]
Read more 2.1.2019 Flying Vehicle Maneuvering Dynamics in Atmosphere with Weight Asymmetry and Elements of Terminal Control in Turn Leg