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  • ISO 15388-2004 - 中外标准 - - 2004/9 - 作废
    ISO 15388:2004 establishes general requirements for contamination and cleanliness control to be applied, at all tiers of supply, to the development of space systems including ground processing facilities, ground support equipment, launch vehicles, spacecraft, payloads, and ground processing and on-orbit operations. It also provides guidelines for the establishment of a contamination and cleanliness control programme.
  • ARINC 750-4-2004 - 中外标准 - - 2004/8 - 现行
  • ISO 15864-2004 - 中外标准 - - 2004/8 - 现行
    ISO 15864:2004 provides the baseline standard on the subject of testing at the system, subsystem, and unit level for applicable unmanned spacecraft programs. It also provides the requirements for documentation associated with testing activities. The acceptance criteria, specifications or procedures, and other detail test requirements applicable to a particular program are defined in the applicable technical specifications and statement of work. When requirements have to be verified by measuring product performance and function under various simulated environments, the method is referred to as "Test." The requirements of ISO 15864:2004 may be tailored for each specific space program application.
    验收检验航空航天运输电磁兼容性航天飞行器运行能力航天运输规范(验收)合格试验振动试验条件方位检验性能要求机上设备航天器航天安全热试验物理性能不载人的磁场声学试验定义试验质量保证设计监督(认可)Acceptance inspectionAcoustic testingAerospace transportBoard outfitDefinitionDefinitionsDesignElectromagnetic compatibilityEMCInspectionMagnetic fieldsOperating abilityOrientationPerformance requirementsPhysical propertiesQualification testsQuality assuranceSpace safetySpace transportSpace vehiclesSpacecraftSpecification (approval)Surveillance (approval)TestingTesting conditionsThermal testingUnmannedVibration
  • ISO 15859-5-2004 - 中外标准 - - 2004/6 - 现行
    ISO 15859-5:2004 specifies limits for the chemical composition and physical properties of nitrogen tetroxide (N2O4)-based propellants and establishes the sampling and test requirements applicable for the verification of the nitrogen tetroxide composition. ISO 15859-5:2004 is applicable to N2O4-based propellants, used as oxidizers in propellant systems of space systems as well as in both flight hardware and ground facilities, systems, and equipment, of types NTO (N2O4 with red-brown colour), MON-1 (N2O4 and NO with green colour), MON-3 (N2O4 and NO with green colour), MON-10 (N2O4 and NO with green colour) and MON-25 (N2O4 and NO with green colour) as well as grades standard (no iron requirement) and low-iron (0,5 microgram per gram or 1,0 microgram per gram iron maximum). ISO 15859-5:2004 is applicable to influents only within the specified limits herein. ISO 15859-5:2004 is applicable to any sampling operation required to ensure that, when the fluid enters the launch vehicle or spacecraft, the fluid composition complies with the limits provided hereafter or with any technical specification agreed to for a particular use.
    流体特性规范航天运输分类系统试验航空航天运输杂质四氧化氮燃料化学成分航空燃料航天器定义推进剂Aerospace transportAviation fuelsChemical compositionClassification systemsDefinitionDefinitionsFluidsFuelsImpuritiesNitrogen tetroxidePropellantsPropertiesSpace transportSpacecraftSpecificationTesting
  • ISO 15859-1-2004 - 中外标准 - - 2004/6 - 现行
    ISO 15859-1:2004 specifies the limit values for the composition of oxygen and establishes the sampling and test requirements applicable for the verification of the oxygen composition. ISO 15859-1:2004 is applicable to oxygen used in both flight hardware and ground facilities, systems and equipment, of the following types and grades: Type I, gaseous (Grade A: standard, purging/pressurization, Grade CB: crew breathing, Grade F: fuel-cell) and Type II, liquid (Grade A: oxidize, Grade B: oxidizer, Grade F: fuel-cell). ISO 15859-1:2004 is applicable to influents only to the extent specified herein. ISO 15859-1:2004 is applicable to any sampling operation required to ensure that, when the fluid enters the launch vehicle or spacecraft, the fluid composition complies with the limits provided hereafter or with any technical specification agreed for a particular use.
    航空航天运输流体特性规范航天运输分类系统试验杂质化学成分定义航天器Aerospace transportChemical compositionClassification systemsDefinitionDefinitionsFluidsImpuritiesOxygenPropertiesSpace transportSpacecraftSpecificationTesting
  • ISO 15859-7-2004 - 中外标准 - - 2004/6 - 现行
    ISO 15859-7:2004 specifies limits for the composition and physical properties of anhydrous hydrazine (N2H4) and establishes the sampling and test requirements applicable for the verification of the anhydrous hydrazine composition. ISO 15859-7:2004 is applicable to anhydrous hydrazine propellant, intended for use as fuel in propellant systems of space systems as well as in both flight hardware and ground facilities, systems, and equipment, of grades: standard [normal production and quality control (suitable for most uses)], monopropellant [normal product with strict control of specified impurities (to be specified only for monopropellant catalytic engines where extended life of the catalyst is desired)] and high purity (special production with strict control of specified impurities). ISO 15859-7:2004 is applicable to influents only within the specified limits herein. Hydrazine may be of the liquid type. ISO 15859-7:2004 is applicable to any sampling operation required to ensure that, when the fluid enters the launch vehicle or spacecraft, the fluid composition complies with the limits provided hereafter or with any technical specification agreed to for a particular use.
    航天器联氨推进剂航空燃料化学成分燃料杂质试验分类系统规范特性航天运输航空航天运输流体定义Aerospace transportAviation fuelsChemical compositionClassification systemsDefinitionDefinitionsFluidsFuelsHydrazineImpuritiesPropellantsPropertiesSpace transportSpacecraftSpecificationTesting
  • ISO 15859-11-2004 - 中外标准 - - 2004/6 - 现行
    ISO 15859-11:2004 specifies limits for the composition of ammonia (NH3) and establishes the sampling and test requirements applicable for the verification of the ammonia composition. ISO 15859-11:2004 is applicable to sampling and test methods for ammonia used in both flight hardware and ground support facilities, systems, and equipment. ISO 15859-11:2004 is applicable to ammonia influents only within the specified limits herein. ISO 15859-11:2004 is applicable to any sampling operation required to ensure that, when the fluid enters the launch vehicle or spacecraft, the fluid composition complies with the limits provided hereafter or with any technical specification agreed to for a particular use.
    航空航天运输流体分类系统试验特性规范定义航天运输化学成分航空燃料燃料杂质航天器Aerospace transportAmmoniaAviation fuelsChemical compositionClassification systemsDefinitionDefinitionsFluidsFuelsImpuritiesPropertiesSpace transportSpacecraftSpecificationTesting
  • ISO 15859-6-2004 - 中外标准 - - 2004/6 - 现行
    ISO 15859-6:2004 specifies limits for the composition of monomethylhydrazine and establishes the sampling and test requirements applicable for the verification of the monomethylhydrazine (MMH) composition. ISO 15859-6:2004 is applicable to monomethylhydrazine propellant, used as a fuel in propellant systems of space systems as well as in both flight hardware and ground facilities, systems, and equipment, of Grade A (98,0 % pure) and Grade F (98,5 % pure). ISO 15859-6:2004 is applicable to influents only within the specified limits herein. ISO 15859-6:2004 is applicable to any sampling operation required to ensure that, when the fluid enters the launch vehicle or spacecraft, the fluid composition complies with the limits provided hereafter or with any technical specification agreed to for a particular use.
    定义流体航空航天运输航天运输特性规范分类系统试验杂质甲基燃料化学成分航空燃料推进剂联氨航天器Aerospace transportAviation fuelsChemical compositionClassification systemsDefinitionDefinitionsFluidsFuelsHydrazineImpuritiesMethylPropellantsPropertiesSpace transportSpacecraftSpecificationTesting
  • ISO 15859-2-2004 - 中外标准 - - 2004/6 - 现行
    ISO 15859-2:2004 specifies limits for the composition of hydrogen and establishes the sampling and test requirements applicable for the verification of the hydrogen composition. ISO 15859-2:2004 is applicable to hydrogen used in both flight hardware and ground facilities, systems and equipment, of the following types and grades: Type I, gaseous (Grade A: fuel, Grade F: fuel) and Type II, liquid (Grade A: fuel, Grade F: fuel). ISO 15859-2:2004 is applicable to influents only to the extent specified. ISO 15859-2:2004 is applicable to any sampling operation required to ensure that, when the fluid enters the launch vehicle or spacecraft, the fluid composition complies with the limits provided hereafter or with any technical specification agreed to for a particular use.
    航天器化学成分定义杂质燃料航空燃料试验分类系统航天运输规范特性流体航空航天运输Aerospace transportAviation fuelsChemical compositionClassification systemsDefinitionDefinitionsFluidsFuelsHydrogenImpuritiesPropertiesSpace transportSpacecraftSpecificationTesting
  • ISO 15859-8-2004 - 中外标准 - - 2004/6 - 现行
    ISO 15859-8:2004 specifies limits for the composition of kerosine and establishes the sampling and test requirements applicable for the verification of the kerosine composition. ISO 15859-8:2004 is applicable to kerosine propellants sampling and test methods for used in both flight hardware and ground support facilities, systems, and equipment. ISO 15859-8:2004 may be applied to influent or effluent kerosine. ISO 15859-8:2004 is applicable to any sampling operation required to ensure that, when the fluid enters the launch vehicle or spacecraft, the fluid composition complies with the limits provided hereafter or with any technical specification agreed to for a particular use.
    定义流体航空航天运输航天运输特性规范分类系统试验杂质燃料化学成分航空燃料煤油推进剂航天器Aerospace transportAviation fuelsChemical compositionClassification systemsDefinitionDefinitionsFluidsFuelsImpuritiesKerosinePropellantsPropertiesSpace transportSpacecraftSpecificationTesting
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