GUO Liang, ZHANG Xu-sheng, HUANG Yong etc. Applications and development of space heat switches in spacecraft thermal control[J]. Editorial Office of Optics and Precision Engineering, 2015,23(1): 216-229
GUO Liang, ZHANG Xu-sheng, HUANG Yong etc. Applications and development of space heat switches in spacecraft thermal control[J]. Editorial Office of Optics and Precision Engineering, 2015,23(1): 216-229 DOI: 10.3788/OPE.20152301.0216.
Applications and development of space heat switches in spacecraft thermal control
Space Heat Switches (SHSs) have wider and important applications in thermal control fields of deep space detectors
space coolers and some spacecrafts. This paper overviews heat transfer mechanisms of SHSs and their structures
key techniques and the advantages and disadvantages of every kind SHSs. Then it reports research progress of the SHSs in recent years
summarizes existing researching work and points out the developing directions of the SHSs. Finally
the authors suggest that those SHSs with high switch ratios and high reliability will be the research emphasis in future because they work at different conditions and require different thermal conductivities
also because the field of space exploration has been extended continuously. Moreover
some component manufacturing and material preparing technologies related to the SHSs will receive much attention
such as the development of new type of drivers
new thermal control coatings and their treatment processes as well as the precision machining and assembly technologies of components.
关键词
Keywords
references
CHO J H. Design, fabrication, and characterization of a MEMS thermal switch and integration with a dynamic micro heat engine[D]. Washington State University, 2007.
郭亮, 吴清文, 黄勇, 等. 空间热开关的研究进展[C]. 第十一届空间热物理会议, 北京, 2013. GUO L, WU Q W, HUANG Y, et al.. Progress of study on space heat switch[C]. 11th Space Thermophysics Conference, Beijing, Nov, 2013. (in Chinese)
闵桂荣, 郭舜. 航天器热控制[M]. 第二版,北京:科学出版社, 1998: 201-204. MIN G R, GUO SH. Spacecraft Thermal Control [M]. Second Edition,Beijing:Science Press, 1998: 201-204. (in Chinese)
VICKERS J M F, GARIPAY R R. Thermal design evolution and performance of the surveyor spacecraft [J]. AIAA, 1968:68-1029.
THEODORE F M, DAVID N G. Development of the viking mars lander thermal control subsystem design [J]. J. Spacecraft, 1968, 13(4): 229-236.
BUGBY D, MARLAND B, STOUFFER C, et al.. Advanced components and techniques for cryogenic integration [J]. AIAA, 2003-344.
王美芬, 闫涛, 洪国同, 等. 微膨胀型低温热开关研究 [J]. 低温工程, 2006(2): 54-57. WANG M F, YAN T, HONG G T, et al.. Experimental research on a practical cryogenic heat switch [J]. Cryogenics, 2006(2): 54-57. (in Chinese)
韩冬, 吴清文, 卢锷, 等. 多姿态变化相机中CCD焦面组件的热设计 [J]. 光学 精密工程, 2009, 17(11): 2665-2671. HAN D, WU Q W, LU E, et al.. Thermal design of CCD focal plane assemblies for attitude-varied space cameras [J]. Opt. Precision Eng., 2009, 17(11): 2665-2671. (in Chinese)
FERNANDO H M, MARCIA B H M. Theoretical and experimental studies of a bi-metallic heat switch for space applications [J]. International Journal of Heat and Mass Transfer, 2003, 46: 4573-4586.
张利, 何兴伟, 黄志光, 等. 空间低温热开关技术的研究进展 [J]. 红外, 2008, 29(7): 15-19. ZHANG L, HE X W, HUANG ZH G, et al.. State-of-arts of space-borne cryogenic thermal switches [J]. Infrared, 2008, 29(7): 15-19. (in Chinese)
ERIC S, KURT L, MIKE P, et al.. Wax-actuated heat switch for Mars surface applications [J]. CP608, Space Technology and Applications International Forum-STAIF, 2002: 211-213.
KETITH S N, CHARLES J P, GAJANAN C B, et al.. Development of a thermal control architecture for the Mars exploration rovers[C].CP654, Space Technology and Applications International Forum-STAIF, 2003: 194-205.
WILLIAMS A D. Robust satellite thermal control using forced air convection thermal switches for operationally responsive space missions[D]. B.S., Texas A & M University, 2002.
KRISHNAN B. Design, fabrication and testing of a shape memory alloy based cryogenic thermal con-duction switch[D]. University of Central Florida, 2004.
张文千. 航天器用记忆合金热开关的设计与理论分析[J]. 真空与低温, 2009, 15(1): 41-44. ZHANG W Q. Design and theoretical analyzes of shape memory alloy heat switch for spaceflight [J]. Vacuum & Cryogenics, 2009, 15(1): 41-44. (in Chinese)
仙石健. 热开关装置: 中国, CN1221200. 1999. XIAN SH J. Thermal switch device:China, CN1221200[P].1999. (in Chinese)
BEASLEY M A, FIREBAUGH S L, EDWARDS R L. MEMS thermal switch for spacecraft thermal control[C]. Janson S. W, Henning A. K. MEMS/MOEMS Components and Their Application, Bellingham, WA: Proceedings of SPIE, 2004.
SLATER T, GERWEN P V, MASURE E, et al.. Thermo-mechanical characteristics of a thermal switch[C]. The 8th International Cofference on Solid-States Sensors and Actuators, and Eurosensors IX, Stock-holm, Sweden, June,1995:25-29.
王熙元, 陈学康, 曹生珠, 等. 卫星静电热开关辐射散热器热性能分析[J]. 真空与低温, 2009, 15(1): 25-29. WANG X Y, CHEN X K, CAO SH ZH, et al.. Thermal performance analysis of electrostatic switched radiator for satellite [J]. Vacuum & Cryogenics, 2009, 15(1): 25-29. (in Chinese)
曹生珠, 陈学康, 王熙元, 等. 微型星用可变辐射器[J]. 真空与低温, 2013, 33(8): 751-754. CAO SH ZH, CHEN X K, WANG X Y, et al.. Novel type of micro-variable radiator for spacecraft thermal control [J]. Vacuum & Cryogenics, 2013, 33(8): 751-754. (in Chinese)
CHO J H, RICHARDS R F, BAHR D F, et al.. Effi-ciency of energy conversion by piezoelectrics [J]. Appl. Phys. Lett.,2006, 89:104107.
JOSHI C, TAI C, MAVANUR A. Heat switch: US, 2005283230. 2005.
向艳超, 彭方汉, 邵兴国. 空间热开关技术的发展现状[C]. 第八届空间热物理会议论文集, 南昌, 2007年9月. XIANG Y CH, PENG F H, SHAO X G. Current status and research development of space heat switch technique[C]. 8th Space Thermophysics Conference, Nanchang, Sep, 2007. (in Chinese)
DAVID G GILMORE. Spacecraft Thermal Control Handbook Volume I: Fundamental Technologies [M]. 2nd Ed,The Aerospace Press, El Segundo, CA, 2002.
王兆利, 李亚丽, 罗宝军, 等. 空间吸附制冷技术的研究进展[J]. 低温工程, 2012, (6): 57-61. WANG ZH L, LI Y L, LUO B J, et al.. Research and development of space sorption cryocooler [J]. Cryogenics, 2012, (6): 57-61. (in Chinese)
CATARINO I, BONFAIT G, DUBAND L. Neon gas-gap heat switch [J]. Cryogenics, 2008, 48: 17-25.
ZHAO B ZH, WANG Q L, LI L K, et al.. Prac-tical application of gas-gap thermal switch in con-duction cooled superconducting magnet system [J]. IEEE Transactions on Applied Super-conductivity, 2012,22(3).
MARLAND B, BUGBY D, STOUFFER C. Development and testing of advanced cryogenic thermal switch concepts [J]. Space Technology and Applications International Forum, Proceedings of a Conference, January, 2000, 504:837-846.
JEONG S H, WATARU N, LEE S K. Experimental investigation of a heat switch based on the precise regulation of a liquid bridge [J]. Applied Thermal Engineering,2012, 39: 151-156.
GONG J, CHA G, JU Y S. Thermal switches based on coplanar EWOD satellite thermal control [J]. MEMS, 1: 13-17, 2008.
ARIC L, MCLANAHAN R. The design, modeling, fabrication, and characterization of an EWOD actuated microthermal switch[D]. Washington State University, 2011.
HO P C, HALLOCK R B. A compact design for an in-dium heat switch [J]. Journal of Low Temperature Physics, 2000,121(5/6): 797-802.
BARTLETT J, HARDY G, HEPBURN I, et al.. Thermal cha-racterization of a tungsten magnetoresistive heat switch [J]. Cryogenics, 2010,50: 647-652.
张加迅, 侯增祺. CPL技术在空间飞行器上的应用 [J]. 工程热物理学报, 2001, 22(3): 340-343. ZHANG J X, HOU Z Q. The application of CPL technique in spacecraft [J]. Journal of Engineering Thermophysics, 2001, 22(3): 340-343. (in Chinese)
MAYDANIK Y F. Loop heat pipes [J]. Applied Thermal Engineering, 2005, 25(5-6): 635-657.