EN 16603-20-08:2014
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
Space engineering - Part 20-08: Photovoltaic assemblies and components
28-02-2015
27-08-2014
Foreword
Introduction
1 Scope
2 Normative references
3 Terms, definitions and abbreviated
terms
4 General
5 Photovoltaic assemblies
6 Solar cell assemblies
7 Bare solar cells
8 Coverglasses
9 Solar cell protection diodes
10 Sun simulators and calibration procedures
11 Capacitance measurement methods
Annex A (normative) - Source control drawing
for photovoltaic assembly (SCD-PVA) - DRD
Annex B (normative) - Source control drawing for solar
cell assembly (SCD-SCA) - DRD
Annex C (normative) - Source control drawing for bare
solar cell (SCD-BSC) - DRD
Annex D (normative) - Source control drawing for coverglass
(SCD-CVG) - DRD
Annex E (normative) - Source control drawing for External
Protection Diodes (SCD-EPD) - DRD
Annex F (normative) - Process identification document (PID)
- DRD
Annex G (normative) - Data documentation package (DDP)
- DRD
Bibliography
This Standard specifies the general requirements for the qualification, procurement, storage and delivery of photovoltaic assemblies, solar cell assemblies, bare solar cells, coverglasses and protection diodes suitable for space applications.This standard does not cover the particular qualification requirements for a specific mission. This Standard primarily applies to qualification approval for photovoltaic assemblies, solar cell assemblies, bare solar cells, coverglasses and protection diodes, and to the procurement of these items.This standard is limited to crystaline Silicon and single and multi-junction GaAs solar cells with a thickness of more than 50 m and does not include thin film solar cell technologies and poly-crystaline solar cells.This Standard does not cover the concentration technology, and especially the requirements related to the optical components of a concentrator (e.g. reflector and lens) and their verification (e.g. collimated light source).This Standard does not apply to qualification of the solar array subsystem, solar panels, structure and solar array mechanisms.This standard may be tailored for the specific characteristic and constrains of a space project in conformance with ECSS-S-ST-00.
Committee |
CEN/CLC/JTC 5
|
DocumentType |
Standard
|
PublisherName |
Comite Europeen de Normalisation
|
Status |
Withdrawn
|
Standards | Relationship |
DS EN 16603-20-08 : 2014 | Identical |
DIN EN 16603-20-08:2014-11 | Identical |
BS EN 16603-20-08:2014 | Identical |
UNI CEI EN 16603-20-08 : 2015 | Identical |
CEI UNI EN 16603-20-08 : 1ED 2016 | Identical |
NS EN 16603-20-08 : 2014 | Identical |
NBN EN 16603-20-08 : 2014 | Identical |
I.S. EN 16603-20-08:2014 | Identical |
NF EN 16603-20-08 : 2016 | Identical |
PN EN 16603-20-08 : 2014 | Identical |
NEN EN 16603-20-08 : 2014 | Identical |
ONORM EN 16603-20-08 : 2014 | Identical |
UNE-EN 16603-20-08:2014 | Identical |
PNE-FprEN 16603-20-08 | Identical |
I.S. EN 16603-10-03:2014 | SPACE ENGINEERING - TESTING |
I.S. EN 16603-10-12:2014 | SPACE ENGINEERING - METHOD FOR THE CALCULATION OF RADIATION RECEIVED AND ITS EFFECTS, AND A POLICY FOR DESIGN MARGINS |
I.S. EN 16602-70-53:2015 | SPACE PRODUCT ASSURANCE - MATERIALS AND HARDWARE COMPATIBILITY TESTS FOR STERILIZATION PROCESSES |
BS EN 16603-10-12:2014 | Space engineering. Method for the calculation of radiation received and its effects, and a policy for design margins |
UNI EN 16603-20-06 : 2014 | SPACE ENGINEERING - SPACECRAFT CHARGING |
BS EN 16603-10-03:2014 | Space engineering. Testing |
BS EN 16602-70-53:2015 | Space product assurance. Materials and hardware compatibility tests for sterilization processes |
EN 16603-20-06:2014 | Space engineering - Spacecraft charging |
EN 16602-70-53:2015 | Space product assurance - Materials and hardware compatibility tests for sterilization processes |
EN 16603-10-12:2014 | Space engineering - Method for the calculation of radiation received and its effects, and a policy for design margins |
BS EN 16603-20-06:2014 | Space engineering. Spacecraft charging |
EN 16603-10-03:2014 | Space engineering - Testing |
UNI EN 16603-10-12 : 2014 | SPACE ENGINEERING - METHOD FOR THE CALCULATION OF RADIATION RECEIVED AND ITS EFFECTS, AND A POLICY FOR DESIGN MARGINS |
I.S. EN 16603-20-06:2014 | SPACE ENGINEERING - SPACECRAFT CHARGING |
EN 16602-70-26:2014 | Space product assurance - Crimping of high-reliability electrical connections |
EN 16602-70-06:2014 | Space product assurance - Particle and UV radiation testing for space materials |
MIL-M-13508 Revision C:1973 | MIRROR, FRONT SURFACED ALUMINIZED: FOR OPTICAL ELEMENTS |
EN 16602-30-11:2014 | Space product assurance - Derating - EEE components |
EN 16602-70:2016 | Space product assurance - Materials, mechanical parts and processes |
EN 16602-30-02:2014 | Space product assurance - Failure modes, effects (and criticality) analysis (FMEA/FMECA) |
ISO 2859:1974 | Sampling procedures and tables for inspection by attributes |
ISO 9211-4:2012 | Optics and photonics Optical coatings Part 4: Specific test methods |
MIL-PRF-13830 Revision B:1997 | Optical Components for Fire Control Instruments; General Specification Governing the Manufacture, Assembly, and Inspection of |
EN 16602-70-09:2015 | Space product assurance - Measurements of thermo-optical properties of thermal control materials |
ISO 23038:2006 | Space systems Space solar cells Electron and proton irradiation test methods |
EN 1939:2003 | Self adhesive tapes - Determination of peel adhesion properties |
IEC 60749-26:2013 | Semiconductor devices - Mechanical and climatic test methods - Part 26: Electrostatic discharge (ESD) sensitivity testing - Human body model (HBM) |
EN 16601-00-01:2015 | Space systems - Glossary of terms |
EN 16602-10-09:2014 | Space product assurance - Nonconformance control system |
ISO 14644-1:2015 | Cleanrooms and associated controlled environments Part 1: Classification of air cleanliness by particle concentration |
EN 16602-70-08:2015 | Space product assurance - Manual soldering of high-reliability electrical connections |
MIL-E-12397 Revision B:1954 | ERASER, RUBBER-PUMICE (FOR TESTING COATED OPTICAL ELEMENTS) |
EN 16602-20-07:2016 | Space product assurance - Quality and safety assurance for space test centres |
ISO 15387:2005 | Space systems Single-junction solar cells Measurements and calibration procedures |
DIN 53289:1979-09 | TESTING OF ADHESIVES FOR METALS AND ADHESIVELY BONDED METAL JOINTS; FLOATING ROLLER PEEL TEST |
EN 16602-70-02:2014 | Space product assurance - Thermal vacuum outgassing test for the screening of space materials |
EN 16602-70-13:2015 | Space product assurance - Measurements of the peel and pull-off strength of coatings and finishes using pressure-sensitive tapes |
EN 16602-60:2015 | Space product assurance - Electrical, electronic and electromechanical (EEE) components |
EN 16603-20-06:2014 | Space engineering - Spacecraft charging |
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