4.1.2017 Basic Selection Criteria of Heat-Resistant and Thermal Protective Structures for High-Altitude Hypersonic Flying Vehicle

Aerodynamic Heating and Thermal Protection of Intercontinental Ballistic Missiles / F. Missile armaments , ( Missile armaments , no. Missile armaments, [...]

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

Numerical simulation of missile warhead operation / G. Missile armaments , ( Missile armaments , no. Missile armaments, vol. Missile armaments [...]

5.1.2019 Methodology of Normative Principles of Justification of Launch Vehicle Launching Facility Structures Lifetime

Missile Armaments. Missile armaments , ( Missile armaments , no. Missile armaments, vol. Missile armaments Том: 2019 Випуск: 2019, (1) Рік: 2019 [...]

4.1.2019 Mathematic Modeling and Investigation into Stress-Strain State of Space Rocket Bays

2019, (1); 21-27 DOI: https://doi.org/10.33136/stma2019.01.021 Language: Russian Annotation: This paper presents the overview and features of the stress-strain state analysis of the [...]

23.1.2019 Calculation of Thermal-Physical Properties of Gaseous Xenon

Missile Armaments. Missile armaments , ( Missile armaments , no. Missile armaments, vol. Missile armaments Том: 2019 Випуск: 2019, (1) Рік: 2019 [...]

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

Missile guidance and control systems. Tactical and Strategic missile guidance. Advances in missile guidance, control, and estimation / S. Missile [...]

8.1.2016 Assessment of Validity of Hypothesis of Constancy of Specific Vacuum Thrust Pulse during SRM Designing and Testing

2016 (1); 55-58 Language: Russian Annotation: In the phase of designing and developmental testing of short-range missiles with main solid rocket motors, the necessity arises [...]

9.1.2023 Methodology for selecting design parameters of solid-propellant sustainer engines. Mathematical support and software

2023 (1); 77-87 DOI: https://doi.org/10.33136/stma2023.01.077 Language: Ukrainian Annotation: Substantiation of the research tools has been performed as a part of methodology [...]

7.1.2023 Specificity of using rubbers as structural materials for making connector assemblies of temperature conditioning systems

Space technology Missile armaments: sb. Space technology Missile armaments: sb. Missile armaments , ( Missile armaments , no. Missile armaments, [...]

3.1.2023 Analysis of a modernized 9K51 Hrad Multiple Rocket Launcher System to determine the performance specifications of the 122-mm unguided rocket projectile in development

Authors observed the importance of reconstruction and upgrading of multiple launch rocket systems of Grad 9К51, Hurricane 9К57 and Tornado 9К58 types and missiles they use by [...]

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4.1.2017 Basic Selection Criteria of Heat-Resistant and Thermal Protective Structures for High-Altitude Hypersonic Flying Vehicle

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

5.1.2019 Methodology of Normative Principles of Justification of Launch Vehicle Launching Facility Structures Lifetime

4.1.2019 Mathematic Modeling and Investigation into Stress-Strain State of Space Rocket Bays

23.1.2019 Calculation of Thermal-Physical Properties of Gaseous Xenon

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

8.1.2016 Assessment of Validity of Hypothesis of Constancy of Specific Vacuum Thrust Pulse during SRM Designing and Testing

9.1.2023 Methodology for selecting design parameters of solid-propellant sustainer engines. Mathematical support and software

7.1.2023 Specificity of using rubbers as structural materials for making connector assemblies of temperature conditioning systems

3.1.2023 Analysis of a modernized 9K51 Hrad Multiple Rocket Launcher System to determine the performance specifications of the 122-mm unguided rocket projectile in development