Aerodynamic design of a descent vehicle in the Martian atmosphere under the exomars project-Reference-Cited by-同舟云学术

Aerodynamic design of a descent vehicle in the Martian atmosphere under the exomars project

Published:2014-11-15 Issue:7 Volume:48 Page:541-548
ISSN:0038-0946
Container-title:Solar System Research
language:en
Short-container-title:Sol Syst Res

Author:

Golomazov M. M.,Finchenko V. S.

Publisher

Pleiades Publishing Ltd

Subject

Space and Planetary Science,Astronomy and Astrophysics

Link

http://link.springer.com/content/pdf/10.1134/S0038094614070089.pdf

Reference10 articles.

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2. Edquist, K.T., Desai, P.N., and Schoenenberger, M., Aerodynamics for the mars phoenix entry capsule, Proc. AIAA/AAS Astrodynamics Specialist Conf. and Exhibit, Washington, August 2008.

3. Golomazov, M.M., Supersonic flow round of segmental and conical bodies by considering chemical reaction, Zh. Vychisl. Mat. Mat. Fiz., 2005, vol. 45, no. 11, pp. 2070–2076.

4. Golomazov, M.M., Finchenko, V.S., Ivankov, A.A., and Shmatov, S.I., Software package for automated design system for apparatuses descending in planetary atmospheres, Vestn. FGUP NPO im. S.A. Lavochkina, 2011, no. 2, pp. 20–25.

5. Golomazov, M.M. and Ivankov, A.A., The way to set boundary conditions at impact wave under flowing round blunt-nosed bodies by hypersonic gas flow, Vestn. FGUP NPO im. S.A. Lavochkina, 2012, no. 1(12), pp. 38–45.

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