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9.1.2023 Methodology for selecting design parameters of solid-propellant sustainer engines. Mathematical support and software
Methodology for selecting design parameters of solid-propellant sustainer engines. The main types of mathematical models, their areas of application have been [...]
Read more 9.1.2023 Methodology for selecting design parameters of solid-propellant sustainer engines. Mathematical support and software
8.1.2024 Theoretic-experimental evaluation of the solid-propellant grain erosive burning
It is typical of the main SRMs of various rocket systems (multiple launch rocket systems, anti-aircraft guided missiles, tactical missiles, boosters). For any point of time [...]
Read more 8.1.2024 Theoretic-experimental evaluation of the solid-propellant grain erosive burning
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 [...]
Read more 13.1.2020 Mathematical models of hydraulic servomechanisms of space technology
5.1.2020 Strength and stability of inhomogeneous structures of space technology, consid-ering plasticity and creep
The main approach in lifetime determination is one that is based on the theory of low-cycle and high-cycle fatigue. Applications of the projective-iterative versions of FEM [...]
Read more 5.1.2020 Strength and stability of inhomogeneous structures of space technology, consid-ering plasticity and creep
12.2.2018 Methodological Support for Initial Phase Optimization of Projecting Design, Trajectory Parameters and Rocket Object Motion Control Programs
The mathematical model of the guided missile provides adequate accuracy for design study to determine: overall dimensions and mass characteristics of the guided missile in general [...]
Read more 12.2.2018 Methodological Support for Initial Phase Optimization of Projecting Design, Trajectory Parameters and Rocket Object Motion Control Programs
7.2.2018 Theoretical Models of Sound Speed Increase Effects in Gas Duct with Corrugated Wall
2018 (2); 57-67 DOI: https://doi.org/10.33136/stma2018.02.057 Language: Russian Annotation: During experimental investigation of the dynamic characteristics of a pneumatic test [...]
Read more 7.2.2018 Theoretical Models of Sound Speed Increase Effects in Gas Duct with Corrugated Wall
13.2.2017 Experience in Development of Isolating Fuel Valve with Pneumatic Drive and Hydraulic Brake for Operation under Cryogenic Conditions
2017 (2); 65-69 Language: Russian Annotation: To support ignition of Taurus LV first stage core structure engine, an oxidizer dividing valve has been developed that ensures [...]
Read more 13.2.2017 Experience in Development of Isolating Fuel Valve with Pneumatic Drive and Hydraulic Brake for Operation under Cryogenic Conditions
1.1.2016 Solid Rocket Motors Developed by DO-5
Language: Russian Annotation: The main phases of formation and development of solid motor engineering are presented.
5.1.2019 Methodology of Normative Principles of Justification of Launch Vehicle Launching Facility Structures Lifetime
Main achievements of Ukrainian scientists in the field of strength and life are specified, taking into account the specifics of various branches of technology. Main [...]
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2.1.2019 Flying Vehicle Maneuvering Dynamics in Atmosphere with Weight Asymmetry and Elements of Terminal Control in Turn Leg
2019, (1); 4-14 DOI: https://doi.org/10.33136/stma2019.01.004 Language: Russian Annotation: This paper suggests method for analysis of the dynamics of the aircraft with weight [...]
Read more 2.1.2019 Flying Vehicle Maneuvering Dynamics in Atmosphere with Weight Asymmetry and Elements of Terminal Control in Turn Leg