Quantitative Thermal Design of Heat Sinks in Large Space Simulators

JIANG Chuan-sheng; WANG Jun

Volume 27 Issue 3

Mar. 2001

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Article Contents

Journal of Beijing University of Aeronautics and Astronautics > 2001 > 27(3): 305-308.

JIANG Chuan-sheng, WANG Jun. Quantitative Thermal Design of Heat Sinks in Large Space Simulators[J]. Journal of Beijing University of Aeronautics and Astronautics, 2001, 27(3): 305-308. (in Chinese)

Citation:

JIANG Chuan-sheng, WANG Jun. Quantitative Thermal Design of Heat Sinks in Large Space Simulators[J]. Journal of Beijing University of Aeronautics and Astronautics, 2001, 27(3): 305-308. (in Chinese)

JIANG Chuan-sheng, WANG Jun. Quantitative Thermal Design of Heat Sinks in Large Space Simulators[J]. Journal of Beijing University of Aeronautics and Astronautics, 2001, 27(3): 305-308. (in Chinese)

Citation:

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Quantitative Thermal Design of Heat Sinks in Large Space Simulators

Beijing University of Aeronautics and Astronautics, Dept. of Flight Vehicle Design and Applied Mechanics

Received Date: 23 Dec 1999
Publish Date: 31 Mar 2001

Abstract

Abstract

The main factors influencing heat sink wall temperature distribution of large space simulators are analyzed. Fin-tube flow rate allocation of heat sinks with different structures are studied with heat sink dynamic simulation software HSDS. Simple and feasible improvements as for thermal design are made to promote the performance of the heat sinks in a large space simulator. Finally, the typical procedure to perform quantitative thermal design of heat sink with HSDS is provided.
- space simulators,
- heat sink,
- simulation,
- thermal design