20.1.2016 Determination of External Characteristic of Autonomous WPP for Regulation by Rotor Withdrawal from under Wind

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19.1.2016 Blade Geometry for Maximal Power Coefficient and Minimal Noise Level

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18.1.2016 Method of Design Evaluation of SRM Lifetime and Ensuring its Long-Term Operation

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17.1.2016 Modeling of Solid Rocket Motor Starting Process

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

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15.1.2016 Calculation of Solid Propellant Grain Burning Surface Using Automated 3D-Modeling Systems

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14.1.2016 Development of Powder Pressure Accumulators for Rocket Cold Start – the Most Important Condition of its Successful Realization

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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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