5.2.2025 Analysis and minimization of resistive forces occurring during rocket stage separation. Possibility of using a single pneumatic pusher for stage separation

Possibility of using a single pneumatic pusher for stage separation Date of receipt of the article for publication: 10.11.2025 Date of acceptance of the article for [...]

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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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