20.2.2017 Research Support for Development of Launch Vehicle Payload Unit Composite Load-Bearing Compartments

By the example of payload fairing and interstage bay of Cyclone-4 launch vehicle, high efficiency is shown of proposed methodology implementation when [...]

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18.2.2017 Development Test of Payload Fairing Separation Dynamics under Ground Conditions

Development Test of Payload Fairing Separation Dynamics under Ground Conditions Authors: Shevtsov E. Fundamentals of Spacecraft Launch Vehicles Designing [...]

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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 [...]

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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

Main advantages of the procedure are its simplicity and versatility since it can be used to determine the acoustic loads around the payload fairings of launch [...]

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