Thermal Analysis Modeling and On-orbit Temperature Prediction for a Microsatellite with Multilayer Insulation
Author:
Affiliation:
1. School of Astronautics, Beihang University
2. The Institute of Manned Space System Engineering, CAST
3. DFH Satellite Co., Ltd., CAST
Publisher
Japan Society for Aeronautical and Space Sciences
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://www.jstage.jst.go.jp/article/tjsass/60/2/60_T-16-21/_pdf
Reference16 articles.
1. 1) Baturkin, V.: Micro-satellites Thermal Control---Concepts and Components, Acta Astronautica, 56 (2005), pp. 161–170.
2. 2) Zhitomirskij, I. S., Kislov, A. M., and Romanenko, V. G.: A Theoretical Model of the Heat Transfer Processes in Multilayer Insulation, Cryogenics, 19 (1979), pp. 265–268.
3. 3) Bapat, S. L., Narayankhedkar, K. G., and Lukose, T. P.: Performance Prediction of Multilayer Insulation, Cryogenics, 30 (1990), pp. 700–710.
4. 4) Krishnaprakas, C. K., Badari Narayana, K., and Dutta, P.: Heat Transfer Correlations for Multilayer Insulation Systems, Cryogenics, 40 (2000), pp. 431–435.
5. 5) Keller, C. W., Cunnington, G. R., and Glassford, A. P.: Thermal Performance of Multilayer Insulations, NASA Report, CR-134477, 1974.
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