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BS EN 16602-60:2015

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by

Space product assurance. Electrical, electronic and electromechanical (EEE) components

Available format(s)

Hardcopy , PDF

Superseded date

14-07-2023

Superseded by

BS EN 16602-60:2023

Language(s)

English

Published date

31-08-2015

€348.24
Excluding VAT

European foreword
Introduction
1 Scope
2 Normative references
3 Terms, definitions and abbreviated terms
4 Requirements for Class 1 components
5 Requirements for Class 2 components
6 Requirements for Class 3 components
7 Quality levels
Annex A (normative) - Component control plan (CCP) - DRD
Annex B (normative) - Declared component list (DCL) - DRD
Annex C (normative) - Procurement specification - DRD
Annex D (normative) - Part approval document (PAD) - DRD
Annex E (informative) - EEE documents delivery per review
Bibliography

Explains the requirements for selection, control, procurement and usage of EEE components for space projects.

Committee
ACE/68
DocumentType
Standard
Pages
102
PublisherName
British Standards Institution
Status
Superseded
SupersededBy

This standard defines the requirements for selection, control, procurement and usage of EEE components for space projects. This standard differentiates between three classes of components through three different sets of standardization requirements (clauses) to be met. The three classes provide for three levels of trade-off between assurance and risk. The highest assurance and lowest risk is provided by class 1 and the lowest assurance and highest risk by class 3. Procurement costs are typically highest for class 1 and lowest for class 3. Mitigation and other engineering measures may decrease the total cost of ownership differences between the three classes. The project objectives, definition and constraints determine which class or classes of components are appropriate to be utilised within the system and subsystems. a. Class 1 components are described in Clause 4. b. Class 2 components are described in Clause 5 c. Class 3 components are described in Clause 6. The requirements of this document apply to all parties involved at all levels in the integration of EEE components into space segment hardware and launchers. This standard may be tailored for the specific characteristics and constraints of a space project in conformance with ECSS-S-ST-00.

Standards Relationship
EN 16602-60:2015 Identical

ISO 14621-1:2003 Space systems Electrical, electronic and electromechanical (EEE) parts Part 1: Parts management
EN 16602-60-13:2015 Space product assurance - Requirements for the use of COTS components
MIL-STD-883 Revision K:2016 TEST METHOD STANDARD - MICROCIRCUITS
EN 16602-30-11:2014 Space product assurance - Derating - EEE components
EN 16602-70:2016 Space product assurance - Materials, mechanical parts and processes
EN 16602-60-05:2014 Space product assurance - Generic procurement requirements for hybrids
EN 16601-40:2014 Space project management - Configuration and information management
EN 16601-10:2015 Space project management - Project planning and implementation
EN 16603-10-04:2015 Space engineering - Space environment
EN 16601-00-01:2015 Space systems - Glossary of terms
EN 16602-60-12:2014 Space product assurance - Design, selection, procurement and use of die form monolithic microwave integrated circuits (MMICs)
EN 16602-10-09:2014 Space product assurance - Nonconformance control system
ISO 14621-2:2003 Space systems Electrical, electronic and electromechanical (EEE) parts Part 2: Control programme requirements
EN 16602-60-02:2014 Space product assurance - ASIC and FPGA development
EN 16602-60-15:2014 Space product assurance - Radiation hardness assurance - EEE components
EN 16602-20:2014 Space product assurance - Quality assurance
EN 16603-10-12:2014 Space engineering - Method for the calculation of radiation received and its effects, and a policy for design margins
EN 16602-60-14:2014 Space product assurance - Relifing procedure - EEE components

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