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47 search results for "gas"
15.1.2024 Enhancing operability of the fuel system units in the hot climate conditions
Heat resistance during compression is most important for rubbers used for seals of various types: rings, collars, armored collars, gaskets for aviation and rocket technology [...]
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7.1.2024 Selection of the functional units for the Cyclone-4M ILV separation system
Brief characteristics of these systems are given, based on the gas-reactive nozzle thrust, braking with solid-propellant rocket engines, separating with spring or pneumatic [...]
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2.1.2024 New and advanced liquid rocket engines of the Yuzhnoye SDO
Over the past 66 years Yuzhnoye SDO has developed more than 40 liquid rocket engines (LRE) of various purpose, designed both to gas-generator cycle and to staged combustion [...]
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10.1.2020 Calculation and selection of parameters for a propellant consumption diagram of dual-thrust main SRM
Gasotermodinamika raketnykh dvigatelei na tverdom toplive.
3.1.2020 Analysis of the unsteady stress-strain behavior of the launch vehicle hold-down bay at liftoff
Stress and deformation of rocket gas turbine disc under different loads using finite element modeling.
19.1.2020 Pyrobolts: types, design, development. Shear type pyrobolt developed at Yuzhnoye SDO
By method of explosive substance action on case structural elements, the pyrobolts are divided into two types: the pyrobolts using the shock wave formed at detonation of brisant [...]
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19.2.2018 Control of Validity and Assessment of Accuracy of Telemetry Results during Full-Scale Test of Launch Vehicles
Use of Statistic Approaches in Analysis of Gas Dynamic Parameters in LV Vented Bays.
12.2.2018 Methodological Support for Initial Phase Optimization of Projecting Design, Trajectory Parameters and Rocket Object Motion Control Programs
Gas Dynamics of Powder Rocket Motors.
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 [...]
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4.2.2018 Turbopump Units of Rocket Engines Developed by DO-4
Having analyzed the data presented, one may conclude that the Rocket Engines Design Office and Yuzhnoye SDO as a whole accumulated sufficient experience and knowledge allowing [...]
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