A highly self-adaptive cold plate for the single-phase mechanically pumped fluid loop for spacecraft thermal management

Author:

Wang Ji-Xiang,Li Yun-Ze,Zhang Hong-Sheng,Wang Sheng-Nan,Liang Yi-Hao,Guo Wei,Liu Yang,Tian Shao-Ping

Funder

National Nature Science Foundation of China

Publisher

Elsevier BV

Subject

Energy Engineering and Power Technology,Fuel Technology,Nuclear Energy and Engineering,Renewable Energy, Sustainability and the Environment

Reference28 articles.

1. Birur GC, Bhandari P, Bame D, Karlmann P, Mastropietro AJ, Liu Y, et al. From concept to flight: an active fluid loop based thermal control system for Mars Science Laboratory Rover. In: 42nd international conf on environmental systems. San Diego, America; July 15–19, 2012.

2. Investigation of a spray cooling system with two nozzles for space application;Wang;Appl Therm Eng,2015

3. An equivalent ground thermal test method for single-phase fluid loop space radiator;Ning;Chin J Aeronaut,2013

4. Investigation of power battery thermal management by using mini-channel cold plate;Huo;Energy Convers Manage,2015

5. Wang J, Li YZ, Wang J. Transient performance investigation of a self-driven adaptive thermostatic valve for single-phase space thermal control loop. In: IEEE/ASME AIM. Wollongong, Australia; July 9–12, 2013. p. 393–98.

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