Designing the configuration and selecting the design parameters of drag systems for deorbiting spacecraft created by pivdenne design office von A. P. Alpatov, E. O. Lapkhanov

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Ballistic Analysis of Orbits Distribution of Spacecraft for Different Missions von A. P. Alpatov, Ju. M. Goldshtejn

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The Development of Structural Design and the Selection of Design Parameters of Aerodynamic Systems for Deorbiting Upper-stage Rocket Launcher von A. P. Alpatov, O. S. Palii, O. D. Skorik

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Development of R&D Fra - mework for the Modernization of the Aerodynamic Deorbit System for the Use in the Upper Stage of Cyclone-1M Launch Vehicle von A. P. Alpatov, O. P. Kuznetsov, O. S. Palii, E. O. Lapkhanov

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