1. Bakulin, V.N., Borzykh, S.V., and Voronin, V.V., Space Vehicle Landing Dynamics at Failure of Landing Gear, Izv.Vuz. Av. Tekhnika, 2016, vol. 59, no. 1, pp. 22–26 [Russian Aeronautics (Engl. Transl.), vol. 59, no. 1, pp. 23–28].
2. Novozhilov, V.V., Teoriya tonkikh obolochrk (Theory of Thin Shells), Leningrad: Sudpromgiz, 1962.
3. Matveenko, A.M. and Nerubailo, B.V., Voprosy prochnosti, ustoichivosti i nadezhnosti konstruktsii (The Issues of Strength, Stability and Reliability of Constructions), Moscow: MAI, 2013.
4. Bakulin V.N. and Potopakhin V.A., Use of the Equations of the Three-Dimensional Elasticity Theory to Solve the Multilayer Shell Dynamics Problems, Izv.Vuz. Av. Tekhnika, 1985, vol. 28, no. 3, pp. 7–12 [Soviet Aeronautics (Engl.Transl.), vol. 28, no. 3, pp. 6–11].
5. Vinogradov, Yu.I. and Bakulin, V.N., Experimental and Analytical Investigation of the Stressed Strained State of a Cylindrical Shell under the Action of Concentrated Radial Forces, Materials Physics and Mechanics, 2016, vol. 26, no. 1, pp. 49–52.