1. Alexashkin, S.N., Ivankov, A.A., and Finchenko, V.S., The way to analyze a temperature state of inflatable braking devices by using the results of flight-designing tests of descending spacecraft “Demonstrator-2R” for clarifying its off-nominal flight, Tepl. Prots. Tekhn., 2009, vol. 1, no. 6, pp. 253–258.
2. Bogdanov, V., Kremnev, R., Rodimov, R., Pitchkhadze, K., Terterashvili, A., and Finchenko, V., On the use of ballute-equipped vehicles for landing on the surface of planets having atmosphere, Proc. 4th Ukraine-Russia-China Symp. of Space Science and Technology, Kiev, 1996, vol. 1, pp. 253–254.
3. Bogdanov, V., Rodimov, R., Pichkhadze, K., Terterashvili, A., Finchenko, V., and Kouznetsov, V., Inflatable ballutes to provide aerodynamic shape to the payload bus enabling its atmosphere entry, Proc. 48th Int. Aeronomical Congress, Turin, Oct. 6–10, 1997.
4. Deryugin, V.A., Pichkhadze, K.M., Finchenko, V.S., and Shmatov, S.I., The way to estimate whether it is possible to descend the spacecrafts from the Earth orbit to the Earth surface, in Rossiiskaya akademiya kosmonavtiki im. K.E. Tsiolkovskogo, NPO im. S.A. Lavochkina: Sbornik nauchnykh trudov (K.E. Tsiolkovskii Russian Academy of Cosmonautics, Lavochkin Association Experimental Design Bureau, Collection of Scientific Papers), Moscow: Blok-Inform-Ekspress, 2000, issue 2, pp. 9–11.
5. Finchenko, V.S., Heat protection of additional inflatable braking devices for the vehicles moving in the atmosphere, Tepl. Prots. Tekhn., 2009a, vol. 1, no. 8, pp. 343–348.