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42 search results for "space launch system"
21.2.2018 Ensuring Aiming Accuracy of Ship’s Telemetry Reception Antenna Installation for Small Vessels
2018 (2); 178-183 DOI: https://doi.org/10.33136/stma2018.02.178 Language: Russian Annotation: For monitoring rocket flight and determining accuracy of spacecraft injection [...]
Read more 21.2.2018 Ensuring Aiming Accuracy of Ship’s Telemetry Reception Antenna Installation for Small Vessels
17.2.2018 Peculiarities of Dynamics of Recoverable Part of Stage of Aircraft-Type Configuration with Turbojet Engine
Analysis of Impact of Flight Scheme of Stage with Rocket-Dynamic Recovery System on Payload Capability of Medium-Class Two-Stage Launch Vehicle. Korolev Samara State [...]
Read more 17.2.2018 Peculiarities of Dynamics of Recoverable Part of Stage of Aircraft-Type Configuration with Turbojet Engine
12.2.2018 Methodological Support for Initial Phase Optimization of Projecting Design, Trajectory Parameters and Rocket Object Motion Control Programs
When trajectory parameters were calculated the missile was regarded as material point of variable mass and the combined equations for center-of-mass motion of the guided missile [...]
Read more 12.2.2018 Methodological Support for Initial Phase Optimization of Projecting Design, Trajectory Parameters and Rocket Object Motion Control Programs
5.2.2018 Electromagnetic Valves Developed by Yuzhnoye SDO Liquid Rocket Engines Design Office
For the European Vega launch vehicle fourth stage main engine assembly that has pressure propellant feeding system, the electrohydraulic valve with amplification and [...]
Read more 5.2.2018 Electromagnetic Valves Developed by Yuzhnoye SDO Liquid Rocket Engines Design Office
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
2.1.2018 Dehydration of Hydrocarbon Fuels by Method of Over-Saturation Drop
Zenit Space Launch System from the Eyes of its Developers / Under the editorship of e.d.
18.2.2017 Development Test of Payload Fairing Separation Dynamics under Ground Conditions
Fundamentals of Spacecraft Launch Vehicles Designing / Under the editorship of V. Method of g-Loads Simulation during Testing of Separation Systems of [...]
Read more 18.2.2017 Development Test of Payload Fairing Separation Dynamics under Ground Conditions
8.1.2017 Initial Imperfection Effect on Loss of Rod Stability under Axial Compression Conditions
On Physical Substantiation of Spontaneous Change of Initial Shape of Extremely Compressed Launch Vehicle Bays. Synergetics: Instability Hierarchies in Self-Organizing [...]
Read more 8.1.2017 Initial Imperfection Effect on Loss of Rod Stability under Axial Compression Conditions
9.1.2019 Modeling of Cyclone-4M Rocket Jet Acoustic Emission by Volumetric Source
2019, (1); 64-71 DOI: https://doi.org/10.33136/stma2019.01.064 Language: Russian Annotation: During lift-off of integrated launch vehicles, the propulsion system jet [...]
Read more 9.1.2019 Modeling of Cyclone-4M Rocket Jet Acoustic Emission by Volumetric Source
6.2.2019 Stabilization of gas reducers adjustment
2019, (2); 42-49 DOI: https://doi.org/10.33136/stma2019.02.042 Language: Russian Annotation: The general information on gas pressure reducers, on their purpose in launch [...]
Read more 6.2.2019 Stabilization of gas reducers adjustment