Effects of active cooling on the metal thermal protection systems

Author:

Liu Shuang,Zhang Boming

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference18 articles.

1. C. Andrew, W. Chivey, M. Maj, et al., Development of an airframe-propulsion integrated generic hypersonic vehicle model, in: 44th AIAA Aerospace Sciences Meeting and Exhibit, AIAA 2006-218, 2006, pp. 9–12.

2. M.A. Bolender, D.B. Doman, Modeling unsteady heating effects on the structural dynamics of a hypersonic vehicle, in: AIAA Atmospheric Flight Mechanics Conference and Exhibit, 2006.

3. M.A. Bolender, D.B. Doman, Modeling unsteady heating effects on the structural dynamics of a hypersonic vehicle, in: AIAA 2006-6646, 2006.

4. J. Buursink, On the development of a cooled metallic thermal protection system for spacecraft, PhD dissertation, TU Delft, 2005.

5. J. Buursink, K.J. Sudmeijer, Experimental studies of an enhanced radiation cooling system, in: Space 2004, Conference and Exhibit, AIAA 2004-5827, 2004.

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