16.1.2020 Parameters of the supersonic jet of a block propulsion system, flowing into a gas duct, considering chemical kinetics of gas-cycle transformations

2020, (1); 149-154 DOI: https://doi.org/10.33136/stma2020.01.149 Language: Russian Annotation: Launch vehicle lift-off is one of the most critical phases of the whole [...]

13.1.2020 Mathematical models of hydraulic servomechanisms of space technology

Using this mathematical model, the powerful actuators of a line of intercontinental ballistic missiles with swinging reentry vehicle and the main engines actuators of Zenit [...]

9.1.2020 Experimental investigation of a liner-free propellant tank made from polymer composite materials

The materials used and propellant tank manufacturing technologies ensure leak-tightness of load-bearing shell at liquid nitrogen operating pressure of 7.5 kgf/cm2 and strength at [...]

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 [...]

21.2.2018 Ensuring Aiming Accuracy of Ship’s Telemetry Reception Antenna Installation for Small Vessels

2018 (2); 178-183 DOI: https://doi.org/10.33136/stma2018.02.178 Language: Russian Annotation: For monitoring rocket flight and determining accuracy of spacecraft injection into the [...]

17.2.2018 Peculiarities of Dynamics of Recoverable Part of Stage of Aircraft-Type Configuration with Turbojet Engine

Analysis of Impact of Flight Scheme of Stage with Rocket-Dynamic Recovery System on Payload Capability of Medium-Class Two-Stage Launch Vehicle.

15.2.2018 Topical Issues of Creation of Space Rocket Thermostatic System Mating Points

Types and Design Features of Thermostating System Mating Points of Launch Vehicle Payload Units and Launch Vehicle and Spacecraft Bays.

13.2.2018 On an Approach to Constructing the Extremes in the Tasks of Optimal Solutions Search

The use of the latter will allow obtaining new solutions of various problems of technical mechanics, such as the task of determining optimal trajectory parameters of launch [...]

12.2.2018 Methodological Support for Initial Phase Optimization of Projecting Design, Trajectory Parameters and Rocket Object Motion Control Programs

Methodological Support for Selection of Launch Vehicle Configuration, Optimization of Design Parameters and Flight Control Programs. Optimization of Super-Light [...]

10.2.2018 Calculation of Gas Flow in High-Altitude Engine Nozzle and Experience of Using Water-Cooled Nozzle Head during Tests

2018 (2); 83-93 DOI: https://doi.org/10.33136/stma2018.02.083 Language: Russian Annotation: At Yuzhnoye State Design Office, the Cyclone-4 launch vehicle 3rd stage [...]