Scope of the Collection

Design and development of components of space launch vehicles and combat missiles (liquid-propellant and solid-propellant rocket engines, propulsion systems, control [...]

3.2.2025 Electric thrusters utilizing metal plasma

A metal plasma rocket engine (Vacuum Arc Thruster, VAT) is a new class of electric propulsion systems in which metal converted into a plasma state using an electric [...]

2.2.2025 Performance analysis and validation of a monopropellant air-detonation ramjet engine

2025 (2); 12-23 DOI: https://doi.org/10.33136/stma2025.02.012 Language: English Annotation: The increasing relevance of alternative propulsion systems necessitates an [...]

5.1.2025 Studying the landing of the reusable first stage of the Cyclone-5 space launch vehicle on a maritime landing platform

A dynamic rocket landing using the primary propulsion system and specialpurpose legs was chosen as the recovery method for the fi rst stage.

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

2024, (1); 61-71 DOI: https://doi.org/10.33136/stma2024.01.061 Language: Ukrainian Annotation: Separation of the spent LV stages is one of the important problems of the [...]

5.1.2024 Assessment of risk of toxic damage to people in case of a launch vehicle accident at flight

Typically, such propellants are used in the LV/ILV upper stages, where a small amount of propellant is contained; however, some LV/ILV still use such fuel in all sustainer [...]

3.1.2024 Future projects of lunar exploration implemented by Yuzhnoye SDO

Based on the analysis of the Lunar Industrial & Research Base conceptual design, such technologies may include rocket propulsion, units and assemblies of [...]

3.1.2020 Analysis of the unsteady stress-strain behavior of the launch vehicle hold-down bay at liftoff

Firstly, the unsteady heat fields on the hold-down bay surface are calculated by means of the semi-empirical method, which is based on the simulated results of the combustion [...]

18.2.2018 Angular Stabilization of an Object Rapidly Rotating around Longitudial Axis

2018 (2); 151-156 DOI: https://doi.org/10.33136/stma2018.02.151 Language: Russian Annotation: Contemporary trends in developing space-rocket hardware indicate the increased [...]

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

This recovery plan differs from an alternative rocket recovery system and, from our point of view, provides more efficient usage of the fuel stores because it doesn’t require [...]