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多层隔热(MLI)结构在高真空环境下具有极低热导率,主要用于太空环境下飞行器和大型燃料贮箱的隔热.本文对MLI结构的隔热原理、选材、制备工艺及应用等进行了综述,简要介绍了国内外MLI结构的研究进展和发展趋势,提出进一步改进MLI的性能是我国实现飞行器长期在轨运行和深空探测的重要研究方向.

参考文献

[1] Hastings L J;Plachta D W;Salerno L .An overview of NASA efforts on zero boil-off storage of cryogenic propellants[J].Cryogenics,2002,41:833-839.
[2] James E;Fesmire S;Augustynowicz D.Cryogenic Thermal Insulation Systems[A].Orlando,Florida,2005:9.
[3] Peterson P ."The Heat-Tight Vessel" A transport and storage vessel for liquid oxygen and liquid nitrogen,etc Translation No.1147[R].Office of Naval Intelligence.University of Lund Sweden,1951.
[4] 张建可,冀勇夫.多层隔热反射屏基底材料试验筛选[J].真空与低温,2007(04):234-236,239.
[5] 江经善.多层隔热材料及其在航天器上的应用[J].宇航材料工艺,2000(04):17-25.
[6] 彭芝生.温控材料之二:隔热及其它材料[A].,1984:84.
[7] 赵玲,吕国志,任克亮,李元林.再入飞行器多层隔热结构优化分析[J].航空学报,2007(06):1345-1350.
[8] Robert J.Stochl;Matthew E.Moran.Multi-Layer Insulation Test Rig for MLI Design Code Validation[A].California:Long Beach,2007:9.
[9] David Plachta;Peter Kittel.An Updated Zero Boil-Off Cryogenic Propellant Storage Analysis Applied to Upper Stages or Depots in an LEO Environment[A].Indiana,2002:7.
[10] Peter E.Glaser.Thermal Protection Systems For Liquid Hydrogen Tanks[M].
[11] 任亚杰.多层隔热体的包扎技术[J].汉中师范学院学报,1999(06):29-32.
[12] 孙慧,徐抒岩,孙守红,曲洪丰.多层隔热组件的制作工艺[J].宇航材料工艺,2011(03):81-83.
[13] Robert J.Stochl;Chinh T.Nguyen.Advanced Insulation Techniques for Cryogenic Tanks[A].Denver,Colorado,2009:8.
[14] James J M .Cryogenic testing of a foam-multilayer insulation concept in a simulated pre-launch environment AIAA 92-3182[R].Nashville,TN,1992.
[15] Kunz O;Renk T;Kauffmann J.FLPP:Cryogenic upper stage technologies programmatic and technological overview[A].
[16] Michael P.Doherty;Joseph D.Gaby;Louis J.Salerno.Cryogenic Fluid Management Technology For Moon and Mars Missions[A].Pasadena,California,2009:9.
[17] Piotr Perczynski;Barry Zandbergen;Juergen Starke.Thermal protection system for long-term in-orbit cryogenic propellant storage[A].Daejeon,Korea,2009
[18] Marlow W A.Design of Multilayer Insulation for the Multipurpose Hydrogen Test Bed[M].American Institute of Aeronautics and Astronautics,2010
[19] Hastings L J;Hedayat A;Brown T M.Analytical modeling and test correlation of variable density multilayer insulation for cryogenic storage[A].
[20] William E.G.Caur D-1T propulsion and propellant systems[A].Nevada,Las Vegas,1973:11.
[21] De Kruif1 J S;Kutter B F.Centaur upper-stage applicability for several-day mission durations with minor insulation modifications[A].Cincinnati,Ohio,2007
[22] Le Bar J F;Cady E C.The advanced cryogenic evolved stage (ACES)-a low-cost,low-risk approach to space exploration launch[A].San Jose,California,U.S.A,2006
[23] 江经善 .实践四号卫星热设计及其实施[J].航天器工程,1995,4(02):46.
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