Analysis of Thermal Protection Using an Anisotropic Material During the Return Capsule Descent

Author:

Zarubin V. S.,Zimin V. N.,Leonov V. V.,Zarubin V. S.

Publisher

Pleiades Publishing Ltd

Subject

Space and Planetary Science,Astronomy and Astrophysics

Reference34 articles.

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2. Chapman, G.T., Theoretical laminar convective heat transfer and boundary layer characteristics on cones at speeds to 24 km/s, NASA Technical Note D-2463, Washington, DC: Natl. Aeronaut. Space Admin., 1964.

3. Efanov, V.V., Martynov, M.B., and Karchaev, Kh.Zh., Aerial vehicles developed at Lavochkin Research and Production Association (On the 80th anniversary of the Lavochkin Association), Sol. Syst. Res., 2018, vol. 52, no. 7, pp. 557–569.

4. Finchenko, V.S., Kotlyarov, E.Yu., and Ivankov, A.A., Sistemy obespecheniya teplovykh rezhimov avtomaticheskikh mezhplanetnykh stantsii (Systems for Providing Thermal Regimes for Automatic Interplanetary Stations), Efanov, V.V. and Finchenko, V.S., Eds., Khimki: NPO im. S.A. Lavochkina, 2018.

5. Finchenko, V.S., Ivankov, A.V., Golomazov, M.M., and Shmatov, S.I., On the use of inflatable decelerators in the design of spacecraft intended for the study of Venus, Sol. Syst. Res., 2020, vol. 54, no. 7, pp. 595–602.

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