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

– New York: Springer-Verlag New York, Inc., 2004.

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6.2.2019 Stabilization of gas reducers adjustment

The brief review of the designs of liquid and bimetal thermal compensators is presented, their advantages and disadvantages are described and the experience of reducers testing with [...]

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