13.1.2019 Prediction of Solid Propellant Burnout Time in Launch Vehicle Propulsion System in Flight

Prediction of Solid Propellant Burnout Time in Launch Vehicle Propulsion System in Flight Authors: Holubek O. Correlation analysis of the realized and nominal dependencies of [...]

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7.1.2024 Selection of the functional units for the Cyclone-4M ILV separation system

cold-launched» separation) is given and their technical substance with advantages and drawbacks is described. Antares – Spaceflight Insider: web site. [...]

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5.1.2020 Strength and stability of inhomogeneous structures of space technology, consid-ering plasticity and creep

The problems of determining the lifetime of space launch vehicles and launching facilities should be noted separately, as it is connected with damages that arise at [...]

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13.1.2018 On Selection of Materials for Creation of Modern LV Thermostating System Mating Hoses

The topical issues are considered of materials designing with consideration for specific features of the hoses as special industrial rubber articles of launch vehicle [...]

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11.1.2019 Peculiarities of Development Testing of Space Rocket Thermostating System Mating Points Hoses

Key words: space launch system , launch site , launch complex , comprehensive development test program , test program and procedure , accelerated [...]

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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

14 CFR, Commercial space transportation, Federal aviation administration, Department of transportation Subchapter C – Licensing, part 420 – License to Operate a Launch [...]

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Сollected book of scientific-technical articles

Subject matter of the collected articles covers the issues of creation and operation of the up-to-date missile and space launch systems, spacecraft and satellite systems, as [...]

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