• Optics and Precision Engineering
  • Vol. 23, Issue 1, 216 (2015)
GUO Liang*, ZHANG Xu-sheng, HUANG Yong, JIANG Fan..., CHEN Li-heng and WANG Zhong-su|Show fewer author(s)
Author Affiliations
  • [in Chinese]
  • show less
    DOI: 10.3788/ope.20152301.0216 Cite this Article
    GUO Liang, ZHANG Xu-sheng, HUANG Yong, JIANG Fan, CHEN Li-heng, WANG Zhong-su. Applications and development of space heat switches in spacecraft thermal control[J]. Optics and Precision Engineering, 2015, 23(1): 216 Copy Citation Text show less
    References

    [1] 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.

    [2] 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)

    [3] MIN G R, GUO SH. Spacecraft Thermal Control [M]. Second Edition, Beijing: Science Press, 1998: 201-204. (in Chinese)

    [4] VICKERS J M F, GARIPAY R R. Thermal design evolution and performance of the surveyor spacecraft [J]. AIAA, 1968: 68-1029.

    [5] THEODORE F M, DAVID N G. Development of the viking mars lander thermal control subsystem design [J]. J. Spacecraft, 1968, 13(4): 229-236.

    [6] BUGBY D, MARLAND B, STOUFFER C, et al.. Advanced components and techniques for cryogenic integration [J]. AIAA, 2003-344.

    [7] 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)

    [8] 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)

    [9] 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.

    [10] 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)

    [11] 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.

    [12] 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.

    [13] 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.

    [14] KRISHNAN B. Design, fabrication and testing of a shape memory alloy based cryogenic thermal con-duction switch [D]. University of Central Florida, 2004.

    [15] 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)

    [16] XIAN SH J. Thermal switch device: China, CN1221200 [P].1999. (in Chinese)

    [17] 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.

    [18] 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.

    [19] 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)

    [20] 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)

    [21] 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.

    [22] JOSHI C, TAI C, MAVANUR A. Heat switch: US, 2005283230 [P]. 2005.

    [23] 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)

    [24] DAVID G GILMORE. Spacecraft Thermal Control Handbook Volume I: Fundamental Technologies [M]. 2nd Ed, The Aerospace Press, El Segundo, CA, 2002.

    [25] 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)

    [26] CATARINO I, BONFAIT G, DUBAND L. Neon gas-gap heat switch [J]. Cryogenics, 2008, 48: 17-25.

    [27] 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).

    [28] 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.

    [29] 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.

    [30] GONG J, CHA G, JU Y S. Thermal switches based on coplanar EWOD satellite thermal control [J]. MEMS, 1: 13-17, 2008.

    [31] ARIC L, MCLANAHAN R. The design, modeling, fabrication, and characterization of an EWOD actuated microthermal switch [D]. Washington State University, 2011.

    [32] 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.

    [33] BARTLETT J, HARDY G, HEPBURN I, et al.. Thermal cha-racterization of a tungsten magnetoresistive heat switch [J]. Cryogenics, 2010, 50: 647-652.

    [34] 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)

    [35] MAYDANIK Y F. Loop heat pipes [J]. Applied Thermal Engineering, 2005, 25(5-6): 635-657.

    CLP Journals

    [1] ZHANG Xu-sheng, GUO Liang, JIA Zhuo-hang, MA Ming-chao, LI Yi, WU Qing-wen. Simulation and experiment of thermal properties for micro-expansion type heat switch with micron stroke[J]. Optics and Precision Engineering, 2016, 24(10): 2442

    GUO Liang, ZHANG Xu-sheng, HUANG Yong, JIANG Fan, CHEN Li-heng, WANG Zhong-su. Applications and development of space heat switches in spacecraft thermal control[J]. Optics and Precision Engineering, 2015, 23(1): 216
    Download Citation