SHEN Zicai , LIU Yuming , TIAN Dongbo , DING Yigang , ZHAO Chunqing , XIA Yan . Standard system for ground simulation test of space environmental effect on space materials[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018 , 39(S1) : 722190 -722190 . DOI: 10.7527/S1000-6893.2018.22190

[1] 沈自才. 空间辐射环境工程[M]. 北京:宇航出版社, 2013:1-3. SHEN Z C. Space radiation environment engineering[M]. Beijing:China Astronautic Publishing House, 2013:1-3(in Chinese).
[2] 沈自才, 丁义刚. 抗辐射设计与辐射效应[M]. 北京:中国科学技术出版社, 2015:13-15. SHEN Z C, DING Y G. Radiation resistance design and radiation effect[M]. Beijing:China Science and Technology Press, 2015:13-15(in Chinese).
[3] 沈自才, 欧阳晓平, 高鸿, 等. 航天材料工程学[M]. 北京:国防工业出版社,2016:109-112. SHEN Z C, OUYANG X P, GAO H, et al. Aerospace material engineering[M]. Beijing:National Defense Industry Press, 2016:119-112(in Chinese).
[4] 冯伟泉,丁义刚, 闫德葵, 等. 空间电子、质子和紫外综合辐照模拟试验研究[J]. 航天器环境工程, 2005, 22(2):69-72. FENG W Q, DING Y G, YAN D K, et al. Study on space electron, proton and ultraviolet combined irradiation simulation test[J]. Spacecraft Environment Engineering, 2005, 22(2):69-72(in Chinese).
[5] 沈自才, 邱家稳, 丁义刚, 等.航天器空间多因素环境协同效应研究[J].中国空间科学技术, 2012, 32(5):54-60. SHEN Z C, QIU J W, DING Y G, et al. Space environment synergistic effect on spacecraft[J].Chinese Space Science and Technology, 2012, 32(5):54-60(in Chinese).
[6] 邱家稳, 沈自才, 肖林.航天器空间环境协同效应研究[J]. 航天器工程, 2013, 22(1):15-20. QIU J W, SHEN Z C, XIAO L. Study on synergistic effect of space environments on spacecraft[J]. Spacecraft Engineering, 2013, 22(1):15-20(in Chinese).
[7] European Cooperation for Space Standardization. Space product assurance-Thermal vacuum outgassing test for the screening of space materials:ECSS-Q-ST-70-02C[S]. Noordwijk:ESA Publications Division, 2008:1-45.
[8] National Aeronautics and Space Administration. Outgassing test for nonmetallic materials associated with sensitive optical surfaces in a space environment:MSFC-SPEC-1443A[S]. Huntsville:Marshall Space Flight Center, 2003:1-11.
[9] ASTM International. Standard test method for contamination outgassing characteristics of spacecraft materials:ASTM E 1559-09[S]. New York:ASTM International, 2009:1-11.
[10] ASTM International. Standard test method for total mass loss and collected volatile condensable materials from outgassing in a vacuum environment:ASTM E 595-15[S]. New York:ASTM International, 2015:1-9.
[11] 国防科学技术工业局. 真空中材料质量损失测试方法:QJ 1322A-2014[S]. 北京:中国航天标准化研究所, 2014:1-12. National Defense Science and Technology Industry Bureau. Test method for mass loss of materials in vacuum:QJ 1322A-2014[S]. Beijing:China Institute of Spaceflight Standardization, 2014:1-12(in Chinese).
[12] 国防科学技术工业局. 航天器用非金属材料真空出气评价方法:QJ 20290-2014[S]. 北京:中国航天标准化研究所, 2014:1-10. National Defense Science and Technology Industry Bureau. Evaluating method of spacecraft nonmetal materials outgassing in vacuum:QJ 20290-2014[S]. Beijing:China Institute of Spaceflight Standardization, 2014:1-12(in Chinese).
[13] 国防科学技术工业局. 真空条件下材料挥发性能测试方法:QJ 1558B-2016[S]. 北京:中国航天标准化研究所, 2016:1-10. National Defense Science and Technology Industry Bureau. Test method for materials outgassing performance in vacuum:QJ 1558B-2016[S]. Beijing:China Institute of Spaceflight Standardization, 2016:1-10(in Chinese).
[14] 中华人民共和国航空航天工业部. 真空-紫外辐照材料质量损失测试方法:QJ 1991-90[S]. 北京:中国航天标准化研究所, 1990:1-6. Ministry of Aeronautics and Astronautics of People's Republic of China. Test method for mass loss of materials irradiated by vacuum ultraviolet:QJ 1991-90[S]. Beijing:China Institute of Spaceflight Standardization, 1990:1-6(in Chinese).
[15] European Cooperation for Space Standardization. Space product assurance-Thermal testing for the evaluation of space materials, processes, mechanical parts and assemblies:ECSS-Q-ST-70-04C[S]. Noordwijk:ESA Publications Division, 2008:1-25.
[16] 国防科学技术工业委员会. 航天器热控涂层试验方法第8部分:热循环试验:GJB 2502.8-2006[S]. 北京:国防科工委军标出版发行部,2006:1-5. National Defense Science and Technology Industry Committee. Test method for thermal control coatings of spacecraft Part 8:Thermal cycle test:GJB 2502.8-2006[S]. Beijing:The Publishing and Issuing Department of the Military Standard of the National Defense Department, 2006:1-5(in Chinese).
[17] European Cooperation for Space Standardization. Space product assurance-Flammability testing for the screening of space materials:ECSS-Q-ST-70-21C[S]. Noordwijk:ESA Publications Division, 2010:1-48.
[18] International Organization for Standardization. Space systems-Space environment-Simulation guidelines for radiation exposure of non-metallic materials:ISO/DIS 15856:2010[S]. Geneva:International Organization for Standardization, 2010:1-32.
[19] National Standards Committee of the Soviet Union. Polimeric materials,methods of radiation tests:GOST 25645.323[S]. Moscow:Standard Press, 1988:1-44.
[20] National Standards Committee of Russia. Polymeric materials for space technique. Requirements for ultraviolet radiation stability tests:GOST R 25645.338[S]. Moscow:Standard Press, 1996:1-16
[21] 国防科学技术工业委员会. 航天器热控涂层试验方法第5部分:真空-紫外辐照试验:GJB 2502.5-2006[S]. 北京:国防科工委军标出版发行部,2006:1-6. National Defense Science and Technology Industry Committee. Test method for thermal control coatings of spacecraft Part 5:Ultraviolet irradiation test in vacuum:GJB 2502.5-2006[S]. Beijing:The Publishing and Issuing Department of the Military Standard of the National Defense Department, 2006:1-6(in Chinese).
[22] 国防科学技术工业委员会. 航天器热控涂层试验方法第6部分:真空-质子辐照试验:GJB 2502.6-2006[S]. 北京:国防科工委军标出版发行部,2006:1-7. National Defense Science and Technology Industry Committee. Test method for thermal control coatings of spacecraft Part 6:Proton irradiation test in vacuum:GJB 2502.6-2006[S]. Beijing:The Publishing and Issuing Department of the Military Standard of the National Defense Department, 2006:1-7(in Chinese).
[23] 国防科学技术工业委员会. 航天器热控涂层试验方法第7部分:真空-电子辐照试验:GJB 2502.7-2006[S]. 北京:国防科工委军标出版发行部,2006:1-7. National Defense Science and Technology Industry Committee. Test method for thermal control coatings of spacecraft Part 7:Electron irradiation test in vacuum:GJB 2502.7-2006[S]. Beijing:The Publishing and Issuing Department of the Military Standard of the National Defense Department, 2006:1-7(in Chinese).
[24] 国防科学技术工业局. 空间用非金属材料太阳紫外辐射效应试验方法:QJ 20286-2014[S]. 北京:中国航天标准化研究所, 2014:1-12. National Defense Science and Technology Industry Bureau. Test method of solar ultraviolet radiation effect for space non-metallic materials:QJ 20286-2014[S]. Beijing:China Institute of Spaceflight Standardization, 2014:1-12(in Chinese).
[25] 国防科学技术工业局. 空间用非金属材料电离辐射效应试验方法:QJ 20289A-2016[S]. 北京:中国航天标准化研究所, 2016:1-9. National Defense Science and Technology Industry Bureau. Test method for total ionizing radiation effect of spacecraft non-metal materials:QJ 20289A-2016[S]. Beijing:China Institute of Spaceflight Standardization, 2016:1-9(in Chinese).
[26] 国防科学技术工业局. 空间材料电子辐射效应试验方法:QJ 20627-2016[S]. 北京:中国航天标准化研究所, 2016:1-13. National Defense Science and Technology Industry Bureau. Test method of electron radiation effect for space materials:QJ 20627-2016[S]. Beijing:China Institute of Spaceflight Standardization, 2016:1-13(in Chinese).
[27] ASTM International. Standard practices for ground laboratory atomic oxygen interaction evaluation of materials for space applications:ASTM E2089-14[S]. New York:ASTM International, 2014:1-5.
[28] MINTON T K. Protocol for atomic oxygen testing of materials in ground-based facilities:NASA CR-197332[R]. Washington, D.C.:NASA, 1994.
[29] 国防科学技术工业委员会. 航天器热控涂层试验方法第9部分:原子氧试验:GJB 2502.9-2006[S]. 北京:国防科工委军标出版发行部,2006:1-6. National Defense Science and Technology Industry Committee. Test method for thermal control coatings of spacecraft Part 9:Atomic oxygen test:GJB 2502.9-2006[S]. Beijing:The Publishing and Issuing Department of the Military Standard of the National Defense Department, 2006:1-6(in Chinese).
[30] 国家国防科学技术工业局. 空间材料原子氧效应试验方法:QJ 20285-2014[S]. 北京:中国航天标准化研究所, 2014:1-10. National Defense Science and Technology Industry Bureau. Test method of atomic oxygen effect for spacecraft materials:QJ 20285-2014[S]. Beijing:China Institute of Spaceflight Standardization, 2014:1-10(in Chinese).
[31] International Organization for Standardization. Space systems-Space solar panels-Spacecraft charging induced electrostatic discharge test methods:ISO 11221:2011[S]. Geneva:International Organization for Standardization, 2011:1-50.
[32] European Cooperation for Space Standardization. Space engineering-Spacecraft charging:Environment-induced effects on the electrostatic behaviour of space systems ECSS-E-ST-20-06C[S]. Noordwijk:ESA Publications Division, 2008:1-120.
[33] National Aeronautics and Space Administration. Low earth orbit spacecraft charging design standard:NASA STD-4005[S]. Washington, D.C.:NASA, 2007.
[34] National Aeronautics and Space Administration. Low earth orbit spacecraft charging design handbook:NASA-HDBK-4006[R]. Washington, D.C.:NASA, 2012.
[35] CAROLYN K P, HENRY B G, WHITTLESEY A C, et al. Design guidelines for assessing and controlling spacecraft charging effects:NASA TP-2361[R]. Washington, D.C.:NASA, 1984.
[36] National Aeronautics and Space Administration. Mitigating in-space charging effects-A guideline:NASA-HDBK-4002A[R]. Washington, D.C.:NASA, 2011.
[37] International Organization for Standardization. Space systems-Space solar cells-Electron and proton irradiation test methods:ISO 23038:2018[S]. Geneva:International Organization for Standardization, 2018:1-10.
[38] International Organization for Standardization. Test procedure to evaluate spacecraft material ejecta upon hypervelocity impact:ISO 11227:2012[S]. Geneva:International Organization for Standardization, 2012:1-23.
[39] 国防科学技术工业局. 航天器空间碎片撞击风险评估程序:QJ 20134-2012[S]. 北京:中国航天标准化研究所,2012:1-24. National Defense Science and Technology Industry Bureau. Risk assessment procedures for spacecraft against space debris impact:QJ 20134-2012[S]. Beijing:China Institute of Spaceflight Standardization, 2012:1-24(in Chinese).
[40] International Organization for Standardization. Space systems-Space environment simulation for material tests-General principles and criteria:ISO 17851:2016[S]. Geneva:International Organization for Standardization, 2016:1-24.
[41] International Organization for Standardization. Space systems-Measurements of thermo-optical properties of thermal control materials:ISO 16378:2013[S]. Geneva:International Organization for Standardization, 2013:1-36.
[42] ASTM International. Standard practice for combined, simulated space environment testing of thermal control materials with electromagnetic and particulate radiation:ASTM E512-94[S]. New York:ASTM International, 2015:1-9.
[43] European Cooperation for Space Standardization. Space product assurance-Particle and UV radiation testing for space materials:ECSS-Q-ST-70-06C[S]. Noordwijk:ESA Publications Division, 2008:1-28.
[44] 国防科学技术工业委员会. 航天器热控涂层试验方法第10部分:综合辐照试验:GJB 2502.10-2006[S]. 北京:国防科工委军标出版发行部,2006:1-7. National Defense Science and Technology Industry Committee. Test method for thermal control coatings of spacecraft Part 10:Combined irradiation test:GJB 2502.10-2006[S]. Beijing:The Publishing and Issuing Department of the Military Standard of the National Defense Department, 2006:1-7(in Chinese).
[45] 国防科学技术工业局. 空间材料综合辐射效应试验方法:QJ 20628-2016[S]. 北京:中国航天标准化研究所,2016:1-18. National Defense Science and Technology Industry Bureau. Test method of combined radiation effects for space materials:QJ 20628-2016[S]. Beijing:China Institute of Spaceflight Standardization, 2016:1-12(in Chinese).
[46] 国防科学技术工业局. 航天器热控材料粒子和紫外综合环境效应试验方法:QJ 20288A-2016[S]. 北京:中国航天标准化研究所, 2016:1-11. National Defense Science and Technology Industry Bureau. Test method for particle and ultraviolet radiation combined effects of spacecraft thermal control materials:QJ 20288A-2016[S]. Beijing:China Institute of Spaceflight Standardization, 2016:1-11(in Chinese).
[47] 国防科学技术工业局. 空间材料原子氧与紫外综合环境试验方法:QJ 20287-2014[S]. 北京:中国航天标准化研究所, 2014:1-12. National Defense Science and Technology Industry Bureau. Test method of atomic oxygen and ultraviolet radiation synergistic effects for spacecraft materials:QJ 20287-2014[S]. Beijing:China Institute of spaceflight Standardization, 2014:1-12(in Chinese).
[48] 国防科学技术工业局. 空间材料原子氧与热循环综合环境模拟试验方法:QJ 20629-2016[S]. 北京:中国航天标准化研究所, 2016:1-12. National Defense Science and Technology Industry Bureau. Test method of atomic oxygen and thermal cycling synergistic effect for spacecraft materials:QJ 20629-2016[S]. Beijing:China Institute of Spaceflight Standardization, 2016:1-12(in Chinese).
[49] 国防科学技术工业局. 空间材料原子氧与带电粒子综合环境模拟试验方法:QJ 20630-2016[S]. 北京:中国航天标准化研究所,2016:1-17. National Defense Science and Technology Industry Bureau. Test method of atomic oxygen and energetic particles synergistic effect for spacecraft materials:QJ 20630-2016[S]. Beijing:China Institute of Spaceflight Standardization, 2016:1-17(in Chinese).