1. Osnovy teploperedachi v aviatsionnoi i raketno-kosmicheskoi tekhnike (Fundamentals of Heat Transfer in Aeronautical and Space Technologies), Avduevskii, V.S. and Koshkin, V.K., Eds., Moscow: Mashinostroenie, 1992.
2. Nikitin, P.V., Teplovaya zashchita (Thermal Protection), Moscow: MAI, 2006.
3. Surzhikov, S.T., Raschetnoe issledovanie aerotermodinamiki giperzvukovogo obtekaniya zatuplennykh tel na primere analiza eksperimental’nykh dannykh (Numerical Simulation of Aerothermodynamic Properties of the Hypersonic Flow over Blunted Bodies: Analysis of Experimental Data), Moscow: IPMekh RAN, 2011.
4. Antuf’ev, B.A. and Konovalov, A.V., Effect of Heating on the Dynamic Behavior of a Shell with Partially Damaged Thermal Insulation, Izv. Vuz. Av. Tekhnika, 2014, vol. 57, no. 1, pp. 3–6 [Russian Aeronautics (Engl. Transl.), vol. 57, no. 1, pp. 1–5].
5. Urazbakhtin, F.A., Kharinova, Yu.Yu., and Urazbakhtin, V.F., A Mathematical Model of Heat Shielding for a Nose Cone Taking into Account Critical Flight Situations, Izv. Vuz. Av. Tekhnika, 2014, vol. 57, no. 1, pp. 73–77 [Russian Aeronautics (Engl. Transl.), vol. 57, no. 1, pp. 100–106].