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19 search results for "Launch vehicle flight"
2.1.2023 How Yuzhnoye develops models for flight safety index evaluation for the case of a rocket failure during the flight
The integral component of this problem along with the safety of operations during launch vehicle ground pre-launch processing is organization of flight [...]
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13.1.2020 Mathematical models of hydraulic servomechanisms of space technology
...of a future hydraulic actuator, selecting optimal characteristics of slides based on specified degree of stability and response of servo actuator and conducting final modeling of [...]
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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 [...]
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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.
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.
9.1.2019 Modeling of Cyclone-4M Rocket Jet Acoustic Emission by Volumetric Source
The modeling of integrated launch vehicle propulsion system (ILV PS) jet acoustic field as bulky radiation source was performed in the rocket flight leg where [...]
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8.2.2019 Evaluation of the external acoustic loads, acting on the rocket when it passes the leg with maximum velocity head
Procedure under consideration is based on the semi-empirical dependency of characteristics of the wideband aerodynamic noise, which occurs during the launch vehicle [...]
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Сollected book of scientific-technical articles
design and development of the launch-vehicles/integrated launch vehicles, missiles, ground complexes; – design and development of the components parts [...]
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