Simulation Study of Active Thermal Control Performance for On-Orbit Space Shuttle

Author:

Yang Chenbing,Pang Liping,Ma Desheng

Publisher

Springer Nature Singapore

Reference7 articles.

1. Bond, T.A., Metcalf, J.L., Asuncion, C.: Shuttle orbiter active thermal control subsystem design and flight experience. SAE Transactions, pp. 804–825 (1991)

2. Nason, J.R., Wierum, F.A., Yanosy, J.L.: Challenges in the development of the orbiter active thermal control subsystem. In: NASA. Johnson Space Center Space Shuttle Technical Conference, Pt. 1 (1985)

3. Oren, J.A., Howell, H.R.: Space station heat rejection subsystem radiator assembly design and development. SAE Transactions 1086–1095 (1995)

4. Anderson, B.J., Justus, C.G., Batts, G.W.: Guidelines for the selection of near-earth thermal environment parameters for spacecraft design (2001)

5. Solare Bestrahlungsstärke: Zusammensetzung einer Messreihe von 1978 bis zur Gegenwart, official website of World Radiation Center in Davos Switzerland. https://www.pmodwrc.ch/?s=solar+constant. 1 Aug 2023

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