IEC PAS 62500-2006 - 中外标准 - - 2006/11 - 作废
Specifies the targets assigned to highly accelerated tests, their basic principle, their scope of application and their implementation procedures. Is a methodological document aimed at facilitating drafting of the specification and then performance of highly accelerated tests by programme managers.
ISO 11076-2006 - 中外标准 - - 2006/11 - 作废
ISO 11076:2006 establishes the minimum requirements for aircraft de-icing/anti-icing methods on the ground, in accordance with the ICAO Manual of aircraft ground de-icing/anti-icing operations and relevant national regulations, to facilitate the safe operation of transport aircraft during icing conditions. This International Standard does not specify requirements for specific aircraft model types. Frost, ice or snow deposits, which can seriously affect the aerodynamic performance and/or controllability of an aircraft, are effectively removed by the application of the procedures specified in ISO 11076:2006. De-icing/anti-icing by mechanical means is not covered by this International Standard.
航空航天运输航空运输飞行器定义除霜解冻剂流体冻结搬运除冰保护液体维修方法人员合格航天运输规范(验收)试验训练利用Aerospace transportAir transportAircraftDefinitionDefinitionsDefrostingDe-icersFluidsFreezingHandlingIcing preventivesLiquidsMaintenanceMethodsPersonnelQualificationsSpace transportSpecification (approval)TestingTrainingUtilization
ISO 23038-2006 - 中外标准 - - 2006/10 - 作废
ISO 23038:2006 specifies the requirements for electron and proton irradiation test methods of space solar cells. It addresses only test methods for performing electron and proton irradiation of space solar cells and not the method for data analysis.
航空航天运输航空运输定义电子束辐射技术测量光线疗法质子辐射太阳能电池太阳能太空技术航天安全航天技术航天运输试验Aerospace transportAir transportDefinitionDefinitionsElectron beamsIrradiation techniqueMeasurementPhototherapyProtonsRadiationSolar cellsSolar energySolar technicsSpace safetySpace technologySpace transportTesting
ISO 15860-2006 - 中外标准 - - 2006/8 - 现行
ISO 15860:2006 covers gases (air, nitrogen, helium, and argon) compressed up to 40 MPa used in systems and units of space vehicle launch and technical complexes. ISO 15860:2006 determines compressed gas impurities (mechanical impurities, water vapour, oil, and foreign gases) content measurement methods. It can be used by countries and firms participating in the development, redesign, modernization, and maintenance of space vehicle launch sites and technical complexes.
航空航天运输航空运输生态污染物清洁(度)污染定义现场试验危害气体测量安全安全要求安全性管理航天安全航天运输航天器规范(验收)Aerospace transportAir transportBiocontaminationCleanlinessContaminationDefinitionDefinitionsField testingHazardsMeasurement of gasesSafetySafety requirementsSecurity managementSpace safetySpace transportSpacecraftSpecification (approval)
ISO 21459-2006 - 中外标准 - - 2006/7 - 作废
Proximity space links are defined to be short-range, bi-directional, fixed or mobile radio links, generally used to communicate among probes, landers, rovers, orbiting constellations, and orbiting relays. These links are characterized by short time delays, moderate (not weak) signals, and short, independent sessions. ISO 21459:2006 defines the coding and synchronization sublayer of the Proximity-1 space link protocol. It defines the data unit of this sublayer, i.e. the PLTU. It defines the coding and synchronization mechanisms required for cross support. It also specifies the send and receive side functionality of this sublayer. ISO 21459:2006 does not specify individual implementations or products, implementation of service interfaces within real systems, methods or technologies required to perform the procedures, or management activities required to configure and control the protocol.
传播学传播方式数据交换数据传送编码信息交换信息传递无线电通信链路无线电波无线电通信航空通讯航天安全航天运输同步遥测技术CommunicationCommunication processesData exchangeData transferEncodingInformation interchangeInformation transferRadio linksRadio wavesRadiocommunicationSpace radiocommunicationsSpace safetySpace transportSynchronizationTelemetry
ISO 21460-2006 - 中外标准 - - 2006/7 - 作废
Proximity space links are defined to be short-range, bi-directional, fixed or mobile radio links, generally used to communicate among probes, landers, rovers, orbiting constellations, and orbiting relays. These links are characterized by short time delays, moderate (not weak) signals, and short, independent sessions. ISO 21460:2006 defines the Proximity-1 space link protocol physical layer. The specification for the channel connection process, provision for frequency bands and assignments, hailing channel, polarization, modulation, data rates, and performance requirements are defined in ISO 21460:2006. Currently, the physical layer only defines operations at UHF frequencies for the Mars environment. ISO 21460:2006 does not specify individual implementations or products, implementation of service interfaces within real systems, methods or technologies required to perform the procedures, or management activities required to configure and control the protocol.
ARINC 664P1-1-2006 - 中外标准 - - 2006/6 - 现行
ARINC 618-6-2006 - 中外标准 - - 2006/6 - 现行
ISO 22672-2006 - 中外标准 - - 2006/6 - 作废
The Forward Space Packet (FSP) service is a Space Link Extension (SLE) transfer service that enables a mission to send Space Packets to a spacecraft in sequence-controlled or expedited mode. ISO 22672:2006 defines, in an abstract manner, the FSP service in terms of the operations necessary to provide the transfer service; the parameter data associated with each operation; the behaviours that result from the invocation of each operation; the relationship between, and the valid sequence of, the operations and resulting behaviours. It does not specify individual implementations or products; the implementation of entities or interfaces within real systems; the methods or technologies required to radiate Space Packets to a spacecraft and to acquire telemetry frames from the signals received from that spacecraft for extraction of the Operational Control Field; the methods or technologies required for communications; the management activities necessary to schedule, configure, and control the FSP service.
ISO 23935-2006 - 中外标准 - - 2006/6 - 现行
ISO 23935:2006 specifies the requirements for tests which may be applied to all fluid system components located in zones designated as "fire zones" and built to satisfy the minimum level specified for withstanding fire. It does not relate to withstanding fire outside designated fire zones, nor to flammability requirements, or to those conditions induced by the flame coming from the combustion chamber.
航空航天运输航空运输飞行器飞行器部件定义环境试验耐火性燃烧试验航天运输试验条件Aerospace transportAir transportAircraftAircraft componentsAircraftsDefinitionDefinitionsEnvironmental testingFire resistanceFire testsFlame testSpace transportTesting conditions