DD IEC TS 62396-5 : DRAFT OCT 2008
Withdrawn
View Superseded by
PROCESS MANAGEMENT FOR AVIONICS - ATMOSPHERIC RADIATION EFFECTS - PART 5: GUIDELINES FOR ASSESSING THERMAL NEUTRON FLUXES AND EFFECTS IN AVIONICS SYSTEMS
11-23-2012
10-27-2018
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Withdrawn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 | |
| Supersedes |
| 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 |