3. Part 3 - EEE

This part explains the modelling of EEE components based on the FIDES 2022 methodology.

To improve its applicability in space, it has been customized for the new methodology. This space customization includes general guidance for the adaptation of FIDES 2022 to space applications (e.g. definition of space mission profiles, adaptation of audits and factors to the processes applied in the space industry), as well as recommendations for the modelling of different components, including innovative technologies.

This part contains the following sections:

• 3.1. Scope
• 3.2. Normative references
• 3.3. Terms, definitions and abbreviated terms
• 3.4. Reliability prediction for EEE components and assemblies
• 3.5. Bibliographic references
• 3.6. Annex A : General formulae for EEE components
• 3.7. EEPL list considered for the modelling
• 3.8. Formulae for all families, as proposed in FIDES
• 3.9. Over-stresses
• 3.10. Component placement in the equipment
• 3.11. Annex B : Formulae concerning Capacitors
• 3.12. Annex C: modified questions in the process questionnaire