ISO 17546:2016
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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Space systems — Lithium ion battery for space vehicles — Design and verification requirements
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19-02-2024
English
09-03-2016
ISO 17546:2016 specifies design and minimum verification requirements for lithium ion rechargeable (including lithium ion polymer) batteries for space vehicles.
Lithium ion secondary electrochemical systems use intercalation compounds (intercalated lithium exists in an ionic or quasi-atomic form within the lattice of the electrode material) in the positive and in the negative electrodes.
The focus of this International Standard is on "battery assembly" and cell is described as "component cells" to be harmonized with other industrial standards and regulations.
"Performance"," safety", and "logistics" are the main points of view to specify.
ISO 17546:2016 does not address "disposal" or "recycle"; however, some recommendations regarding disposal are suggested.
Committee |
ISO/TC 20/SC 14
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DevelopmentNote |
Supersedes ISO/DIS 17546. (03/2016)
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DocumentType |
Standard
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Pages |
52
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ProductNote |
THIS STANDARD ALSO REFERS TO ECSS-Q-ST-70C,ECSS-Q-ST-30-11C,ECSS-Q-ST-40-02C,ECSS-E-ST-10-02C,ECSS-E-ST-10-03C,SMC standard SMC-S-017,NASA/TM-2009-2215751:NESC-RP-08-75/06-069-I, JSC20793 rev.B,RCC Document 319-10
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PublisherName |
International Organization for Standardization
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Status |
Superseded
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SupersededBy | |
UnderRevision |
Standards | Relationship |
BS ISO 17546:2016 | Identical |
ISO 10795:2011 | Space systems Programme management and quality Vocabulary |
IEC 62281:2016 | Safety of primary and secondary lithium cells and batteries during transport |
IEC 61960:2011 | Secondary cells and batteries containing alkaline or other non-acid electrolytes - Secondary lithium cells and batteries for portable applications |
MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
ISO 24113:2011 | Space systems Space debris mitigation requirements |
AIAA S 122 : 2007 | ELECTRICAL POWER SYSTEMS FOR UNMANNED SPACECRAFT |
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