DD IEC TS 62396-4 : DRAFT 2008
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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PROCESS MANAGEMENT FOR AVIONICS ATMOSPHERIC RADIATION EFFECTS - PART 4: GUIDELINES FOR DESIGNING WITH HIGH VOLTAGE AIRCRAFT ELECTRONICS AND POTENTIAL SINGLE EVENT EFFECTS
31-10-2013
23-11-2012
FOREWORD
INTRODUCTION
1 Scope
2 Normative references
3 Terms and definitions
4 Potential high voltage single event effects
5 Quantifying single event burnout in avionics for high
voltage devices
6 Relevant SEB data and applying it to avionics
6.1 SEB data from heavy ion testing is not relevant
6.2 SEB data from high energy neutron and proton testing
6.3 Calculating the SEB rate at aircraft altitudes
6.4 Measurement of high voltage component radiation
characteristics, EPICS
7 Conclusion
Bibliography
Gives guidance on atmospheric radiation effects on high voltage (nominally above 200 V) avionics electronics used in aircraft operating at altitudes up to 60000 ft (18,3 km).
| Committee |
GEL/107
|
| DevelopmentNote |
Supersedes DD IEC/PAS 62396-4. (04/2009)
|
| DocumentType |
Draft
|
| PublisherName |
British Standards Institution
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| Standards | Relationship |
| IEC TS 62396-4:2008 | 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 |
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