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Modeling of the plasma environment of re-entry space vehicles. / Shevyrin, Alexander A.; Shkredov, Timofey Yu; Shoev, Georgy V. et al.

19th International Conference on the Methods of Aerophysical Research, ICMAR 2018. ed. / Fomin. Vol. 2027 American Institute of Physics Inc., 2018. 030031 (AIP Conference Proceedings; Vol. 2027).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › Research › peer-review

Harvard

Shevyrin, AA, Shkredov, TY, Shoev, GV & Bondar, YA 2018, Modeling of the plasma environment of re-entry space vehicles. in Fomin (ed.), 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018. vol. 2027, 030031, AIP Conference Proceedings, vol. 2027, American Institute of Physics Inc., 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018, Akademgorodok, Novosibirsk, Russian Federation, 13.08.2018. https://doi.org/10.1063/1.5065125

APA

Shevyrin, A. A., Shkredov, T. Y., Shoev, G. V., & Bondar, Y. A. (2018). Modeling of the plasma environment of re-entry space vehicles. In Fomin (Ed.), 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018 (Vol. 2027). [030031] (AIP Conference Proceedings; Vol. 2027). American Institute of Physics Inc.. https://doi.org/10.1063/1.5065125

Vancouver

Shevyrin AA, Shkredov TY, Shoev GV, Bondar YA. Modeling of the plasma environment of re-entry space vehicles. In Fomin, editor, 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018. Vol. 2027. American Institute of Physics Inc. 2018. 030031. (AIP Conference Proceedings). doi: 10.1063/1.5065125

Author

Shevyrin, Alexander A. ; Shkredov, Timofey Yu ; Shoev, Georgy V. et al. / Modeling of the plasma environment of re-entry space vehicles. 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018. editor / Fomin. Vol. 2027 American Institute of Physics Inc., 2018. (AIP Conference Proceedings).

BibTeX

@inproceedings{affea02d022e458281192e8627ab4b8c,
title = "Modeling of the plasma environment of re-entry space vehicles",
abstract = "Application of the direct simulation Monte Carlo (DSMC) method for calculating the flow near superorbital space vehicles at the high-altitude (above 70 km) part of the trajectory is considered. An example of application of various models of the ionized flow near the vehicle during its reentry into the Earth's atmosphere for calculating the flow of the Stardust sample return capsule (entry speed 12.4 km/s) is presented. The influence of numerical models on the values of convective and radiative heat fluxes is investigated. It is found that the characteristic feature of such high-speed flows is the mutual influence of ionization and radiation processes, which must be taken into account in modeling.",
keywords = "SIMULATION, RADIATION",
author = "Shevyrin, {Alexander A.} and Shkredov, {Timofey Yu} and Shoev, {Georgy V.} and Bondar, {Yevgeny A.}",
note = "Publisher Copyright: {\textcopyright} 2018 Author(s).; 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018 ; Conference date: 13-08-2018 Through 19-08-2018",
year = "2018",
month = nov,
day = "2",
doi = "10.1063/1.5065125",
language = "English",
volume = "2027",
series = "AIP Conference Proceedings",
publisher = "American Institute of Physics Inc.",
editor = "Fomin",
booktitle = "19th International Conference on the Methods of Aerophysical Research, ICMAR 2018",

}

RIS

TY - GEN

T1 - Modeling of the plasma environment of re-entry space vehicles

AU - Shevyrin, Alexander A.

AU - Shkredov, Timofey Yu

AU - Shoev, Georgy V.

AU - Bondar, Yevgeny A.

N1 - Publisher Copyright: © 2018 Author(s).

PY - 2018/11/2

Y1 - 2018/11/2

N2 - Application of the direct simulation Monte Carlo (DSMC) method for calculating the flow near superorbital space vehicles at the high-altitude (above 70 km) part of the trajectory is considered. An example of application of various models of the ionized flow near the vehicle during its reentry into the Earth's atmosphere for calculating the flow of the Stardust sample return capsule (entry speed 12.4 km/s) is presented. The influence of numerical models on the values of convective and radiative heat fluxes is investigated. It is found that the characteristic feature of such high-speed flows is the mutual influence of ionization and radiation processes, which must be taken into account in modeling.

AB - Application of the direct simulation Monte Carlo (DSMC) method for calculating the flow near superorbital space vehicles at the high-altitude (above 70 km) part of the trajectory is considered. An example of application of various models of the ionized flow near the vehicle during its reentry into the Earth's atmosphere for calculating the flow of the Stardust sample return capsule (entry speed 12.4 km/s) is presented. The influence of numerical models on the values of convective and radiative heat fluxes is investigated. It is found that the characteristic feature of such high-speed flows is the mutual influence of ionization and radiation processes, which must be taken into account in modeling.

KW - SIMULATION

KW - RADIATION

UR - http://www.scopus.com/inward/record.url?scp=85056349740&partnerID=8YFLogxK

U2 - 10.1063/1.5065125

DO - 10.1063/1.5065125

M3 - Conference contribution

AN - SCOPUS:85056349740

VL - 2027

T3 - AIP Conference Proceedings

BT - 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018

A2 - Fomin, null

PB - American Institute of Physics Inc.

T2 - 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018

Y2 - 13 August 2018 through 19 August 2018

ER -

ID: 17409258