10.1.2020 Calculation and selection of parameters for a propellant consumption diagram of dual-thrust main SRM

Calculation and selection of parameters for a propellant consumption diagram of dual-thrust main SRM Authors: Yenotov V. The equations obtained show that the required [...]

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8.1.2018 The Solid–Propellant Motors with Regulated Thrust

The Solid–Propellant Motors with Regulated Thrust Authors: Glazkov V. 2018 (1); 46-52 DOI: https://doi.org/10.33136/stma2018.01.046 Language: Russian Annotation: The paper [...]

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5.1.2018 Experimental Determination of Lateral Force Caused by SRM Thrust Vector Eccentricity and Skew

Experimental Determination of Lateral Force Caused by SRM Thrust Vector Eccentricity and Skew Authors: Bezkrovny І. 2018 (1); 27-30 DOI: [...]

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16.1.2016 Peculiarities of Development of SRM Thrust Vector Controls at DO-5

Peculiarities of Development of SRM Thrust Vector Controls at DO-5 Authors: Slisarenko V. 2016 (1); 97-104 Language: Russian Annotation: The thrust vector controls, [...]

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11.1.2016 Methodology of Design Evaluation of Main SRM Flowrate-Thrust Characteristics after Stage Separation

Methodology of Design Evaluation of Main SRM Flowrate-Thrust Characteristics after Stage Separation Authors: Ushkin M. 2016 (1); 68-75 Language: Russian Annotation: The [...]

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

Assessment of Validity of Hypothesis of Constancy of Specific Vacuum Thrust Pulse during SRM Designing and Testing Authors: Kalnysh R. 2016 (1); 55-58 Language: Russian [...]

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2.1.2016 Experience of Testing SRM Thrust Vector Controls

Experience of Testing SRM Thrust Vector Controls Authors: Golubenko M. 2016 (1); 13-18 Language: Russian Annotation: The design peculiarities and basic characteristics of [...]

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2.1.2020 Analysis of development trends of design parameters and basic characteristics of missiles for the advanced multiple launch rocket systems

The mathematical model of the guided missile provides adequate accuracy for design study to determine depending on the main design parameters: overall dimensions and mass [...]

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8.1.2024 Theoretic-experimental evaluation of the solid-propellant grain erosive burning

2024, (1); 72-77 DOI: https://doi.org/10.33136/stma2024.01.072 Language: Ukrainian Annotation: The high demands for the flow rate and thrust characteristics specified for the [...]

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

Brief characteristics of these systems are given, based on the gas-reactive nozzle thrust, braking with solid-propellant rocket engines, separating with spring or pneumatic [...]

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