21.2.2017 Mass Parameter Optimization of Thermal Protective Structure for Reusable Spacecraft

Mass Parameter Optimization of Thermal Protective Structure for Reusable Spacecraft Authors: Husarova I. C., [...]

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6.1.2017 Drought Post-Effects Satellite Monitoring

K., Voloshin V. I., Voloshin V. K., Voloshin V. Content 2017 (1) Downloads: 19 [...]

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7.1.2019 Experience of Development and Use of Generator Pressurization System for Tanks of Launch Vehicles on High-Temperature Propellants

Experience of Development and Use of Generator Pressurization System for Tanks of Launch Vehicles on [...]

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

Opredelenie kolebania davlenia v gazovoy polosti hermetychikh emkostey transportnozapravochnykh [...]

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14.2.2019 Selection of the validation algorithm for the solid rocket motor trust measurement procedure

Selection of the validation algorithm for the solid rocket motor trust measurement procedure Authors: [...]

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4.2.2019 Numerical simulation of behavior of elastic structures with local stiffening elementse

Konechnoelementniy analiz ploskodeformiruemukh sred s vklyucheniyami. Chislennoye modelirovanie povedeniya [...]

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8.1.2023 Specificity of developing pyrobolts with low impact and vibration impulse responses

, Voloshin V. Shevtsov E.I., Voloshin V.V., Samoilenko I.D. Identification of [...]

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2.1.2023 How Yuzhnoye develops models for flight safety index evaluation for the case of a rocket failure during the flight

The basic model for assessing the risks of damage to facilities and people is analyzed, using the maximum impact zone of an [...]

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