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IEC 62396-1

Process management for avionics – Atmospheric radiation effects – Part 1: Accommodation of atmospheric radiation effects via single event effects within avionics electronic equipment

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Organization: IEC
Publication Date: 1 January 2016
Status: active
Page Count: 108
ICS Code (Production. Production management): 03.100.50
ICS Code (Electronic components in general): 31.020
ICS Code (Aerospace electric equipment and systems): 49.060
scope:

This part of IEC 62396 is intended to provide guidance on atmospheric radiation effects on avionics electronics used in aircraft operating at altitudes up to 60 000 ft (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 International Standard is intended to help avionics 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.

Document History

IEC 62396-1
January 1, 2016
Process management for avionics – Atmospheric radiation effects – Part 1: Accommodation of atmospheric radiation effects via single event effects within avionics electronic equipment
This part of IEC 62396 is intended to provide guidance on atmospheric radiation effects on avionics electronics used in aircraft operating at altitudes up to 60 000 ft (18,3 km). It defines the...
May 1, 2012
Process management for avionics – Atmospheric radiation effects – Part 1: Accommodation of atmospheric radiation effects via single event effects within avionics electronic equipment
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...
February 1, 2006
Process management for avionics – Atmospheric radiation effects – Part 1: Accommodation of atmospheric radiation effects via single event effects within avionics electronic equipment
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...

References

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