Experimental study on the transient behaviors of mechanically pumped two-phase loop with a novel accumulator for thermal control of space camera payload-Reference-Cited by-同舟云学术

Experimental study on the transient behaviors of mechanically pumped two-phase loop with a novel accumulator for thermal control of space camera payload

Published:2020-10 Issue: Volume:179 Page:115714
ISSN:1359-4311
Container-title:Applied Thermal Engineering
language:en
Short-container-title:Applied Thermal Engineering

Author:

Meng Qingliang,Zhao Zhenming,Zhang Tao,van Es Johannes,Pauw Aswin,Zhang Huandong,Yan Yinxue

Funder

National Natural Science Foundation of China, China

Shanghai Sailing Program, China

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Energy Engineering and Power Technology

Reference35 articles.

1. Thermal design considerations of the Hubble space telescope (HST) science instrument control and data handler;Gregory,2013

2. Thermal effects in optical systems;Jamieson;Opt. Eng.,1980

3. Analysis of defocusing thermal effects in optical systems;Olivieri;SPIE.,1996

4. Research on space optical remote sensor thermal control technique;Li;J. Astro.,2014

5. Gravity-capillary evaporation regimes in micro-grooves;Zhang;J. AIChE.,2019

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