CEN EN 16602-60 Space product assurance - Electrical, electronic and electromechanical (EEE) components
Данный раздел/документ содержится в продуктах:
- Техэксперт: Машиностроительный комплекс
- Картотека зарубежных и международных стандартов
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- 49
- CEN EN 16602-70-29 Space product assurance - Determination of offgassing products from materials and assembled articles to be used in a manned space vehicle crew compartment
- 49.140
- CEN EN 16602-70-29 Space product assurance - Determination of offgassing products from materials and assembled articles to be used in a manned space vehicle crew compartment
- DIN EN 16602-20-07 Space produce assurance - Quality and safety assurance for space test centres
- DIN EN 16602-20-07 Space produce assurance - Quality and safety assurance for space test centres
- DIN EN 16602-20-07 Space produce assurance - Quality and safety assurance for space test centres
- DIN EN 16602-20-08 Space product assurance - Storage, handling and transportation of spacecraft hardware
- DIN EN 16602-70 Space product assurance - Materials, mechanical parts and processes
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- DIN EN 16602-70-10 Space product assurance - Qualification of printed circuit boards
- CEN EN 16602-20 Space product assurance - Quality assurance
- Картотека зарубежных и международных стандартов
European Committee for Standardization
Space product assurance - Electrical, electronic and electromechanical (EEE) components
N EN 16602-60
Annotation
This European 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.
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