BS EN 16602-60:2015
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by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
Hardcopy , PDF
14-07-2023
English
31-08-2015
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Superseded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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