Design Experience of a Demonstrator Descent Vehicle Introducing Aeroelastic Deployable Structural Elements to Space Engineering-Reference-Cited by-同舟云学术

Design Experience of a Demonstrator Descent Vehicle Introducing Aeroelastic Deployable Structural Elements to Space Engineering

Published:2018-11-29 Issue:7 Volume:52 Page:590-596
ISSN:0038-0946
Container-title:Solar System Research
language:en
Short-container-title:Sol Syst Res

Author:

Alifanov O. M.,Medvedskiy A. L.,Terentyev V. V.,Lyskov D. V.

Publisher

Pleiades Publishing Ltd

Subject

Space and Planetary Science,Astronomy and Astrophysics

Link

http://link.springer.com/content/pdf/10.1134/S0038094618070031.pdf

Reference22 articles.

1. Alifanov, O.M. and Ouchcatov, V.I., Thermal protection of reentry vehicles using inflatable braking devices, Proc. World Space Congr., October 10–19, 2002, Houston, 2002, no. IAC-02-16.03.2002.

2. Alifanov, O.M., Budnik, S.A., and Netelev, A.V., RF Patent 132423, 2013a.

3. Alifanov, O.M., Ivankov, A.A., Netelev, A.V., and Finchenko, V.S., Characteristics of heat protecting coating for aeroelastic braking devices of reentry into planets’ atmosphere, Tr. Mosk. Aviats. Inst., 2013b, no. 71. https://doi.org/mai.ru//upload/iblock/fd3/fd3e5f902a3249cfbcb18820d1789d9c.pdf . Cited February 14, 2017.

4. Alifanov, O.M., Ivankov, A.A., Netelev, A.V., and Finchenko, V.S., Aeroelastic devices with flexible heat protection for spacecrafts braking in planet’s atmosphere, Tepl. Protsessy Tekh., 2014, no. 7, pp. 301–307.

5. Bogdanov, V.V., Kremnev, R.S., Rodimov, R.Yu., Pitchkhadze, K.M., et al., On the use of ballute-equipped vehicles for landing on the surface of planets having atmosphere, Proc. 4th Ukraine-Russia-China Symp. of Space Sciences and Technology, Kiev, 1996, vol. 1, pp. 253–254.

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