BS DD IEC/TS 62396-1-2006
航空电子设备过程管理.大气辐射效应.调节航空电子设备内经单粒子效应的大气辐射作用

Process management for avionics - Atmospheric radiation effects - Accommodation of atmospheric radiation effects via single event effects within avionics electronic equipment

BS DD IEC/TS 62396-1-2006 发布历史

This Technical Specification is intended to provide guidance on Atmospheric Radiation effects on Avionics electronics used in aircraft operating at altitudes up to 60 000 feet (18,3 km). It defines the radiation environment, the effects of that environment on electronics and provides design considerations for the accommodation of those effects within avionics systems. This Technical Specification is intended to help aerospace equipment manufacturers and designers to standardise their approach to Single Event Effects in Avionics by providing guidance, leading to a standard methodology. Details of the radiation environment are provided together with identification of potential problems caused as a result of the atmospheric radiation received. Appropriate methods are given for quantifying Single Event Effect (SEE) rates in electronic components. The overall system safety methodology should be expanded to accommodate the Single Event Effects rates and to demonstrate the suitability of the electronics for the application at the component and system level.

BS DD IEC/TS 62396-1-2006由英国标准学会 GB-BSI 发布于 2006-07-31，并于 2006-07-31 实施。

BS DD IEC/TS 62396-1-2006 在中国标准分类中归属于: V40 电气系统与设备，在国际标准分类中归属于: 49.060 航空航天用电气设备和系统。

BS DD IEC/TS 62396-1-2006的历代版本如下：

• 2006年07月31日 BS DD IEC/TS 62396-1-2006 航空电子设备过程管理.大气辐射效应.调节航空电子设备内经单粒子效应的大气辐射作用

BS DD IEC/TS 62396-1-2006 于 2015-05-31 变更为 BS IEC 62396-1-2012 航空电子设备过程管理.大气辐射效应.调节航空电子设备内经单粒子效应的大气辐射作用。

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标准号

BS DD IEC/TS 62396-1-2006

发布日期

2006年07月31日

实施日期

2006年07月31日

废止日期

无

中国标准分类号

V40

国际标准分类号

49.060

发布单位

GB-BSI

代替标准

BS IEC 62396-1-2012

适用范围

This Technical Specification is intended to provide guidance on Atmospheric Radiation effects on Avionics electronics used in aircraft operating at altitudes up to 60 000 feet (18,3 km). It defines the radiation environment, the effects of that environment on electronics and provides design considerations for the accommodation of those effects within avionics systems. This Technical Specification is intended to help aerospace equipment manufacturers and designers to standardise their approach to Single Event Effects in Avionics by providing guidance, leading to a standard methodology. Details of the radiation environment are provided together with identification of potential problems caused as a result of the atmospheric radiation received. Appropriate methods are given for quantifying Single Event Effect (SEE) rates in electronic components. The overall system safety methodology should be expanded to accommodate the Single Event Effects rates and to demonstrate the suitability of the electronics for the application at the component and system level.

BS DD IEC/TS 62396-1-2006系列标准