13.1.2016 The Impact of Diaphragm’s Shape on Gas Dynamic Flow Characteristics in Small-Size SRM Combustion Chamber

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12.1.2016 Increasing Effectiveness of Meteorological Rockets when Using Hybrid Motors

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

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10.1.2016 Development of Winding Pattern during Calculation of Composite Case Winding Programs

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9.1.2016 Evaluation of SRM Intraballistic Parameters Scatter by Monte-Carlo Method

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

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13.1.2016 The Impact of Diaphragm’s Shape on Gas Dynamic Flow Characteristics in Small-Size SRM Combustion Chamber

12.1.2016 Increasing Effectiveness of Meteorological Rockets when Using Hybrid Motors

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

10.1.2016 Development of Winding Pattern during Calculation of Composite Case Winding Programs

9.1.2016 Evaluation of SRM Intraballistic Parameters Scatter by Monte-Carlo Method

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

7.1.2016 Updated Design of SRM Test Rig

6.1.2016 Ensuring Solid Rocket Motor Moisture Resistance by Design

5.1.2016 Scientific-Technical Base for Creation of Detonation Solid Rocket Motors

2.1.2016 Experience of Testing SRM Thrust Vector Controls