9.2.2016 Metrological Support of Kinematic Model Testing on Zero-Gravity Test Stands

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8.2.2016 Development and Validation of Program Module for Construction of Virtual Models of Real Structures in ANSYS System

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7.2.2016 Analysis of Operation Modes and Selection of Chemical Current Source Included in Autonomous Electric Power Supply Systems of Self-Propelled Launcher

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6.2.2016 Experimental Investigations into Results of Testing Cyclone-4 ILV Thermostating System Mating Points

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5.2.2016 Creation of Technological Tooling and Testing of Cocoon-Type Cases Manufacturing Technology

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4.2.2016 Experimental Investigations of Possibility of Creating Impulse SRM with Short Operation Period

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3.2.2016 Selection of Optimal Trajectories of Spacecraft Launch Vehicles

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

Therewith, the loads can be created that are critical for the launching equipment, rocket body and especially for the spacecraft, which are under the fairing. The maximal [...]

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8.1.2019 Virtual Tests of Cassette Reentry Vehicle Dash Elements Attachment System during Ground Operation

For the specified loading conditions during the ground operations with the warhead, the most dangerous computational cases are determined which have been implemented during [...]

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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

Important role of the gas sprayer design in pressurization system parametric configuration is described, and the advanced versions are shown taking into account g-loads, [...]

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