IEC TS 62396-4:2008

IEC TS 62396-4:2008

July 2008
Technical specification Cancelled

Process management for avionics - Atmospheric radiation effects - Part 4: Guidelines for designing with high voltage aircraft electronics and potential single event effects

IEC/TS 62396-4:2008(E) is intended to provide guidance on atmospheric radiation effects on high voltage (nominally above 200 V) avionics electronics used in aircraft operating at altitudes up to 60 000 ft (18,3 km). To be used in conjunction with IEC/TS 62396-1. Defines the effects of that environment on high voltage electronics and provides design considerations for the accommodation of those effects within avionics systems. Is intended to help aerospace equipment manufacturers and designers to standardise their approach to single event effects on high voltage avionics by providing guidance, leading to a standard methodology.

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International IEC standards

Publication date

July 2008

Number of pages

16 p.

Reference

IEC TS 62396-4:2008

Print number

1 - 19/08/2008
Sumary
Process management for avionics - Atmospheric radiation effects - Part 4: Guidelines for designing with high voltage aircraft electronics and potential single event effects

IEC/TS 62396-4:2008(E) is intended to provide guidance on atmospheric radiation effects on high voltage (nominally above 200 V) avionics electronics used in aircraft operating at altitudes up to 60 000 ft (18,3 km). To be used in conjunction with IEC/TS 62396-1. Defines the effects of that environment on high voltage electronics and provides design considerations for the accommodation of those effects within avionics systems. Is intended to help aerospace equipment manufacturers and designers to standardise their approach to single event effects on high voltage avionics by providing guidance, leading to a standard methodology.
Replaced standards (1)
IEC PAS 62396-4:2007
September 2007
Publicly available specification Cancelled
Process management for avionics - Atmospheric radiation effects - Part 4: Guidelines for designing with high voltage aircraft electronics and potential single event effects

Provides guidance on atmospheric radiation effects on high voltage, nominally above 200 V, avionics electronics used in aircraft operating at altitudes up to 60 000 feet. Is to be used in conjunction with IEC/TS 62396-1. Defines the effects of that environment on high voltage electronics and provides design considerations for the accommodation of those effects within avionics systems.

Standard replaced by (1)
IEC 62396-4:2013
September 2013
International standard Current
Process management for avionics - Atmospheric radiation effects - Part 4: Design of high voltage aircraft electronics managing potential single event effects

IEC 62396-4:2013(E) provides guidance on atmospheric radiation effects and their management on high voltage (nominally above 200 V) avionics electronics used in aircraft operating at altitudes up to 60 000 ft (18,3 km). This part of IEC 62396 defines the effects of that environment on high voltage electronics and provides design considerations for the accommodation of those effects within avionics systems. This part of IEC 62396 provides technical data and methodology for aerospace equipment manufacturers and designers to standardise their approach to single event effects on high voltage avionics by providing guidance, leading to a standard methodology. This publication is to be read in conjunction with IEC 62396-1:2012.

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