9.1.2019 Modeling of Cyclone-4M Rocket Jet Acoustic Emission by Volumetric Source

The maximal acoustic pressure level in 150 Hz frequency in the payload area outside the fairing – 155 dB, in the instrumentation bay area – 157 dB, in the intertank bay area [...]

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6.1.2019 Investigation into Peculiarities of Delivery to Launch Base of Rocket Propellant with Specified Gasing

This procedure implies that shipping tank container is pressurized after being fueled with propellants at the manufacturer’s, the pressure is characterized by the value of [...]

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21.1.2019 Optimization of Geometrical Shape of Isolation Valve Blading Position

With decrease of the pressure losses, the required upstream pressure of the propulsion system is ensured with smaller pressurization of the tanks.

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5.1.2023 Fueling-neutralization stations. New developments and applications

2023 (1); 48-55 DOI: https://doi.org/10.33136/stma2023.01.048 Language: Ukrainian Annotation: The article dwells on development and study of the multifunctional operations while [...]

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1.1.2023 On the development of a methodology for building air and missile defense systems. Explanation of the investigation mechanism

44-48 Ostankov V. 

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