1. Afanas’ev, V.A., Degtyarev, G.L., and Meshchanov, A.S., Parametric Identification of a Return Space Vehicle during Vertical Landing, Izv. Vuz. Av. Tekhnika, 2018, vol. 61, no 1, pp. 26–34 [Russian Aeronautics (Engl. Transl.), vol. 61, no. 1, pp. 23–31].
2. Afanas’ev, V.A., Degtyarev, G.L., and Meshchanov, A.S., Controlling of a Return Space Vehicle along Transition Trajectories in Atmosphere, Izv. Vuz. Av. Tekhnika, 2015, vol. 58, no. 2, pp. 16–22 [Russian Aeronautics (Engl. Transl.), vol. 58, no. 2, pp. 152–159].
3. Velikanova, N.P., Statistical Analysis of Experimental Study Results on Low-Cycle Fatigue Resistance for the EI698-VD High-Temperature Alloy, Izv. Vuz. Av. Tekhnika, 2009, vol. 52, no. 4, pp. 25–28 [Russian Aeronautics (Engl. Transl.), vol. 52, no. 4, pp. 413–418].
4. Nesterov, V.E., Rudakov, V.B., and Makarov, M.I., Development Test Objectives Analysis of Reusable Space Rocket System, Vestnik MAI, 2013, vol. 20, no. 5, pp. 77–85.
5. Nikitin, P.V. and Sotnik, E.V., Reproduction of the Convective-Radiant Heat Exchange Accompanying the Entrance of Space Vehicles in the Atmospheres of Planets at the Second Space Velocity, Trudy MAI, 2011, no. 42, URL: http://trudymai.ru/eng/published.php?ID=24309.