IEC 62396-1:2016 PDF

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 60000 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.

IEC 62396-1:2016 Referenced Document

GEIA-STD-4899A-2007 Standard for Preparing an Electronic Components Management Plan*， 2024-04-20 Update
IEC 62396-2:2012 Process management for avionics - Atmospheric radiation effects - Part 2: Guidelines for single event effects testing for avionics systems
IEC 62396-3:2013 Process management for avionics - Atmospheric radiation effects - Part 3: System design optimization to accommodate the single event effects (SEE) of atmospheric radiation
IEC 62396-4:2013 Process management for avionics - Atmospheric radiatio effects - Part 4: Design of high voltage aircraft electronics managing potential single event effects
IEC 62396-5:2014 Process management for avioncs - Atmospheric radioation effects - Part 5: Assessment of thermal neutron fluxes and single event effects in avionics systems

0000 IEC 62396-1:2016 RLV
2012 IEC 62396-1:2012 Process management for avionics - Atmospheric radioation effects - Part 1: Accommodation of atmospheric radiation effects via single event effects within avionics electronic equipment