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54 search results for "launch vehicle"
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.
15.2.2018 Topical Issues of Creation of Space Rocket Thermostatic System Mating Points
Types and Design Features of Thermostating System Mating Points of Launch Vehicle Payload Units and Launch Vehicle and Spacecraft Bays.
13.2.2018 On an Approach to Constructing the Extremes in the Tasks of Optimal Solutions Search
The use of the latter will allow obtaining new solutions of various problems of technical mechanics, such as the task of determining optimal trajectory parameters of launch [...]
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12.2.2018 Methodological Support for Initial Phase Optimization of Projecting Design, Trajectory Parameters and Rocket Object Motion Control Programs
Methodological Support for Selection of Launch Vehicle Configuration, Optimization of Design Parameters and Flight Control Programs. Optimization of Super-Light [...]
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
2018 (2); 83-93 DOI: https://doi.org/10.33136/stma2018.02.083 Language: Russian Annotation: At Yuzhnoye State Design Office, the Cyclone-4 launch vehicle 3rd stage [...]
Read more 10.2.2018 Calculation of Gas Flow in High-Altitude Engine Nozzle and Experience of Using Water-Cooled Nozzle Head during Tests
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 [...]
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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 [...]
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13.1.2018 On Selection of Materials for Creation of Modern LV Thermostating System Mating Hoses
2018 (1); 72-84 DOI: https://doi.org/10.33136/stma2018.01.072 Language: Russian Annotation: A series of materials is proposed for creation of space launch vehicle [...]
Read more 13.1.2018 On Selection of Materials for Creation of Modern LV Thermostating System Mating Hoses
2.1.2018 Dehydration of Hydrocarbon Fuels by Method of Over-Saturation Drop
URL: https://ru.wikipedia.org/wiki/Soyuz-2_(launch vehicle family) . URL: https://ru.wikipedia.org/wiki/Angara_(launch vehicle) . URL: [...]
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18.2.2017 Development Test of Payload Fairing Separation Dynamics under Ground Conditions
Fundamentals of Spacecraft Launch Vehicles Designing / Under the editorship of V.