On-Orbit Validation of Thermal Control Subsystem for Microsatellite with Integrated Configuration of Platform and Payload

Author:

Wang Jie,Chen Zegui,Fan Caizhi,Wu Guofu,Luo Jiqiang,Feng Maolong

Publisher

Elsevier BV

Subject

General Earth and Planetary Sciences,General Environmental Science

Reference18 articles.

1. Very-small-satellite design for distributed space missions;D J Barnhart;Journal of Spacecraft and Rockets,2007

2. Analysis of platform and payload integrated design technology for optical remote sensing satellites;Y Yao;3rd International symposium of space optical instruments and applications,2017

3. Integrated Design of Platform and Payload for Remote Sensing Satellite;J Zu;International Symposium of Space Optical Instrument and Application,2018

4. Thermal control subsystem requirements and challenges for a responsive satellite bus;A D Williams;Proceedings of SPIE -The International Society for Optical Engineering,2009

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