聚合物基复合材料在液氧贮箱中的应用研究

宇航材料工艺 , 2004, 34(1): 16-22. doi: 10.3969/j.issn.1007-2330.2004.01.004

聚合物基复合材料在液氧贮箱中的应用研究

王戈 ^1, , 刘长军 ^2, , 李效东 ^3, , 李公义 ^4,

1.国防科技大学,航天与材料工程学院CFC重点实验室,长沙,410073

2.国防科技大学,航天与材料工程学院CFC重点实验室,长沙,410073

3.国防科技大学,航天与材料工程学院CFC重点实验室,长沙,410073

4.国防科技大学,航天与材料工程学院CFC重点实验室,长沙,410073

关键词：液氧 , 贮箱 , 相容性 , 聚合物 , 复合材料

Study on Application of Polymer Composites in Liquid Oxygen Tank

回顾了航天系统液氧贮箱的历史沿革,论证聚合物复合材料作为贮箱材料应用的必要性和可行性.从聚合物基体和纤维选择,复合材料的成型,与液氧相容性的评价以及综合性能测试进行了讨论.

参考文献

[1]	Richard J W;Roule G M.Large scale composite liquid oxygen feedlines for launch vehicles[A].,2000:352-359.
[2]	Kim et al.Cyanate ester composites for oxygen containment[P].US 6,334,589,2002.
[3]	Grat N A;Hudgm R;MeBain M .Oxygen compatibility testing of composite materials[Z].N20010020209
[4]	Robinson M J.Composite structure on the DC-XA reuseable launch vehicle[A].,1996:530-541.
[5]	Nihart G J;Smith C P .Compatibility of materials with 7500PSI oxygen[Z].AMRL-TDR-64-76
[6]	Bryan C J.High-pressure liquid and gaseous oxygen impact sensitivity evaluation of materials for use at kennedy space center[M].NASA TN D-8160
[7]	Lowrie R.Heat of combustion and oxygen compatibility[A].ASTM STP 812,American Society for Testing and Materials,1983:84-96.
[8]	Chou T C;Anthony Fiedorowicz.Oxygen compatibility of polymers including TFE-Teflon,Kel-F82,Vespel SP-21,Viton A-500,Fluorel,Neoprene,EPDM,Buna-N,and Nylon 6,6.Royals W T,Chou T C,Steinberg T A eds.Flammability and sensitivity of materials in oxygen-enriched atmospheres:Eighth Volume.ASTM STP 1319[M].American Society for Testing and Materials,1997:319-349.
[9]	Williams M K;Faughnan P D.Characterization of polymers found in an oxygen enviroment[A].ASTM STP 1319,American Society for Testing and Materials,1997:403-409.
[10]	Steinberg T A.Combustion testing of non-metallic materials in ambient and oxygen-enriched atmospheres[A].ASTM STP 1319,American Society for Testing and Materials,1997:84-96.
[11]	Waller J M;Homung S D;Beeson H D.Fuel cell elastomeric materials oxygen compatibility testing:effect of 450 and 6 200 kPa oxygen[A].ASTM STP 1319,American Society for Testing and Materials,1997:385-402.
[12]	Robinson M J;Stoltzfus J M;Owens T N.Composite material compatibility with liquid oxygen[J].AIAA 97-1107:973-982.
[13]	Gudatis C N.High pressure cryogenic composite tank qualification[A].,2000:342-351.
[14]	Vendroux G;AuberonM;Dessaut J.Cryogenic composite tanks:structure analysis and manufacturing concepts[A].,1997:828-838.
[15]	NASA Marshell Space Flight Center .Composite hquid oxygen tank tests successful[OL].http://std.msfc.nasa.gov/news/02tank.html,2001.
[16]	Kim et al.Hybrid composites for oxygen propulsion systems[P].US 6,375,125,2002.
[17]	Delay .Composite tank[P].US:6,158,605,2002.
[18]	Delay .Method of making a composite tank[P].US:6,193,917,2001.
[19]	Grat N A;Schieleit G F;Biggs R .Adhesive bonding characterization of composite joints for cryogenic usage[Z].N20010020380
[20]	Albritton N;Young W .Cryogenic evaluation of epoxy bond strength[J].Cryogenics,1996,36:713-716.
[21]	Ronssy L;Parcelier M.Influence of polymeric matrix and fther on composite materials at low temperatures.ALAA95-6134[A].Chattanooga,1995
[22]	Lee B L;Holl M W .Effects of moisture and thermal cycling on In-plane shear properties of graphite fibre-rinforced cyanate ester resin composites[J].Composites Part A:Applied Science and Manufacturing,1996,27:1015-1022.
[23]	Roylance M;Kirn P.Innovative E-Beam cured structures for aircraft[A].,2001:2515-2525.
[24]	Raghavant J;Lopata V J;Beillie P M.Influence of process parameters on electron beamm curing of a polymer composite[A].,1998:56-167.
[25]	Abrams F.Ananalysis of E-Beam potential in acrospace composite manufacturing[A].In,1997:548.
[26]	Foedingger R.Electron beam curing of filament wound composites pressure vessels[A].,1999:248.
[27]	Flammability,odor,and offgassing requirements and test procedures for materials in environments that support combustion.NASA-NHB 8060[Z].
[28]	Liquid Oxygen Compatibility Impact Sensitivity Test Method.U.S.Air Force Specification Bulletin 527[Z].
[29]	Standard test method for compatibility of materials with liquid oxygen ( impact sensitivity threshold and pass-fail techniques).ASTM D-2512-95[S].
[30]	Steinberg T A.Combustion testing of non-metallic materials in ambient and oxygen-enriched atmosphere[A].SATM STP 1319,American Society for Testing and Materials,1997:370-383.
[31]	BEESON H D;Hshieh Fu Yu;Hirsch D B.Ignitiability of advanced composites in liquid and gaseous oxygen[A].ASTM STP 1319,American Society for Testing and Materials,1997:421-431.

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聚合物基复合材料在液氧贮箱中的应用研究

Study on Application of Polymer Composites in Liquid Oxygen Tank

参考文献