Ground Simulation Testing of Solar Receiver for the Space Station

XING Yu ming; YUAN Xiu gan; CUI Hai ting; HOU Xin bin; WANG Chang he

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Ground Simulation Testing of Solar Receiver for the Space Station

更新时间：2026-07-07

- Ground Simulation Testing of Solar Receiver for the Space Station
- Vol. 17, Issue 2, (2002)
- 作者机构：
  
  北京航空航天大学飞行器与应用力学系,北京,100083
- 作者简介：
- 基金信息：
- DOI：
  CLC：
- Published：2002
- 稿件说明：
移动端阅览
XING Yu ming, YUAN Xiu gan, CUI Hai ting, et al. Ground Simulation Testing of Solar Receiver for the Space Station[J]. 2002, 17(2).
DOI：

XING Yu ming, YUAN Xiu gan, CUI Hai ting, et al. Ground Simulation Testing of Solar Receiver for the Space Station[J]. 2002, 17(2). DOI：

摘要

利用相变材料 (PCM)的熔化潜热来蓄热可以保证空间站太阳能热动力系统在轨道的阴影期内仍能连续发电。针对这一核心技术

建立了空间太阳能吸热 -储热器单元换热器地面模拟实验台。在模拟轨道条件下

对不同入射热流、不同工质进口温度及不同工质流量进行了多种组合测试。结果表明

单管工质气体的出口温升在轨道的日照期和阴影期都达到了预期的要求

相变材料容器的最高温度和平均温度都处于材料的安全范围内。

Abstract

The solar dynamic power module proposed for the space station uses the heat of fusion of a phase change material (PCM) to efficiently store thermal energy for use during eclipse periods.Experimental investigation has been conducted in solar simulation testing for the heat receiver in the Brayton engine used as the solar dynamic option for the space station.This paper discusses solar receiver ground based experiments and analytical heat transfer studies.The hardware

test procedures

and test results from these experiments are discussed.After more than 100 simulated space station orbital cycles

no canister cracks or leaks were observed and all data were successfully collected.The results show that the output temperature of the gas from the working fluid tubes met the expected demand during the sunlight and eclipse periods

the maximum temperature and average temperature of the PCM container were all within the safe range.

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Related Author

XIE Yong-qi

YU Jian-zu

GAO Hong-xia

CHI Peng-tao

RUI Shou-zhen

XING Yu-ming

WU Bin

Frank Dammel

Related Institution

School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics

School of Aeronautical Science and Engineering, Beijing University of Aeronautics and Astronautics

Chair of Technical Thermodynamics, Darmstadt University of Technology

School of Aeronautic Science and Technology, Beijing University of Aeronautics and Astronautics

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