Name: DD IEC TS 62396-5 : DRAFT OCT 2008
Brand: BSI

DD IEC TS 62396-5 : DRAFT OCT 2008

Withdrawn

PROCESS MANAGEMENT FOR AVIONICS - ATMOSPHERIC RADIATION EFFECTS - PART 5: GUIDELINES FOR ASSESSING THERMAL NEUTRON FLUXES AND EFFECTS IN AVIONICS SYSTEMS

Withdrawn date

27-10-2018

Published date

23-11-2012

Publisher

British Standards Institution

1 Scope
2 Normative references
3 Terms and definitions
4 Overview of thermal neutron single event rate calculation
5 Thermal neutron flux inside an airliner
  5.1 Definition of thermal neutron
  5.2 Overview
  5.3 Background on aircraft measurements
  5.4 Calculational approach
  5.5 Processing of in-flight neutron flux data
6 Thermal neutron SEU cross sections
  6.1 Overview of the issue
  6.2 Mechanism involved
  6.3 Thermal neutron SEU cross sections and Ratio-2
7 Recommendation for devices in avionics at present time
Bibliography

Gives a more precise definition of the threat that thermal neutrons pose to avionics as a second mechanism for inducing single event upset (SEU) in microelectronics.

Committee	GEL/107
DevelopmentNote	Supersedes DD IEC PAS 62396-5. (10/2008)
DocumentType	Draft
PublisherName	British Standards Institution
Status	Withdrawn
SupersededBy	BS IEC 62396-5:2014
Supersedes	DD IEC PAS 62396-5 : DRAFT NOV 2007

Standards	Relationship
IEC TS 62396-5:2008	Identical

IEC TS 62396-1:2006

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