Modeling and identification of the processes of heat exchange in porous materials of thermal protection of reusable aerospace systems

被引：2

作者：

Reznik S.V. ^{[1
]}

Fisher W.P.P. ^{[2
]}

Martines D. ^{[3
]}

Paderin L.Ya. ^{[4
]}

Pavlyukevich N.V. ^{[5
]}

Petit D. ^{[6
]}

Prosuntsov P.V. ^{[1
]}

机构：

[1] N. É. Bauman Moscow State Technical University, Moscow, 105005

[2] EADS Space Transportation GmbH Group, Bremen

[3] PSA, Tabernas (Almeria)

[4] N. E. Zhukovskii Central Aerohydrodynamics Institute, Zhukovskii, 140160, Moscow Region

[5] A. V. Luikov Heat and Mass Transfer Institute, National Academy of Sciences of Belarus, Minsk, 220072

[6] École Nationale Supérieure de Mécanique et d'Aérotechnique, Futuroscope Cedex

来源：

Journal of Engineering Physics and Thermophysics | 2004年 / 77卷 / 3期

关键词：

Transportation; Statistical Physic; Heat Exchange; Porous Material; Thermal Protection;

D O I：

10.1023/B:JOEP.0000036492.18328.f2

中图分类号：

学科分类号：

摘要：

The features of aerospace systems as transport facilities for exploration of near-earth space and high-velocity intercontinental transportation have been considered. Problems of complex investigations of the processes of heat exchange in porous materials of thermal protection of prospective reusable aerospace systems have been formulated. © 2004 Plenum Publishing Corporation.

引用

页码：471 / 477

页数：6

共 25 条

[1] Polezhaev Yu.V., Yurevich F.B., Thermal Protection [in Russian], (1976)
[2] Leont'ev A.I., Pilyugin N.N., Polezhaev Yu.V., Polyaev V.M., Scientific Principles of Technologies of the XXIst Century [in Russian], (2000)
[3] Reznik S.V., Materials and Coatings under Extremal Conditions. Insight to the Future, 1, (2002)
[4] Gladkii V.F., The mistery of the project of the R-3 rocket, Aviats. Kosmonavt., 11, pp. 13-16, (2002)
[5] Chernyi I., High-power rockets for the near future, Novosti Kosmonavt., 14, 1, pp. 30-32, (2004)
[6] Feoktistov K.P., Space Techniques. Perspectives of Development [in Russian], (1997)
[7] Lozino-Lozinskii G.E., Bratukhin A.G., Aviation-space Systems [in Russian], (1997)
[8] Gofin M.Ya., Heat-resistant and Thermal-protective Structures of Space Shuttles [in Russian], (2003)
[9] Kelly H.N., Rummler D.R., Jackson L.R., Proc. AIAA/NASA Conf. Adv. Technol. Space Syst.: Collect. Tech. Pap., pp. 12-23, (1979)
[10] Taylor A.H., Cerro J.A., Jackson L.R., Analytical study of reusable flight-weight cryogenic propellant tank designs, Aerokosm. Tekh., 9, pp. 101-111, (1986)

← 1 2 3 →