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BS ISO 17546:2024

BS ISO 17546:2024

$198.66

Space systems. Lithium ion battery for space vehicles. Design and verification requirements

Published By Publication Date Number of Pages
BSI 2024 66
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PDF Catalog

PDF Pages PDF Title
2 undefined
8 Foreword
9 Introduction
11 1 Scope
2 Normative references
3 Terms and definitions
16 4 Symbols and abbreviated terms
5 Cell
5.1 Performance
5.1.1 General
17 5.1.2 Test requirements
5.1.3 Test data trending [4]
18 5.1.4 Cell qualification test
5.1.5 Leakage (hermetic) test
5.1.6 Safety tests
5.1.7 Thermal/thermal vacuum test [5]
5.1.8 Mechanical environmental test
19 5.1.9 Radiation test
5.1.10 Life cycle test
20 5.1.11 Models for analysis
5.2 Safety
5.2.1 General
5.2.2 Hazard description
5.2.3 Protective devices as a hazard control
21 5.2.4 Safety testing
22 5.2.5 Important test considerations
23 5.2.6 Optional test
5.3 Logistics
5.3.1 General
24 5.3.2 Cell manufacturing, storage and testing
5.3.3 Safety measure for handling
25 5.3.4 Cell transportation
5.4 COTS cells for space use
5.4.1 General
5.4.2 Safety requirements
5.4.3 Lot integrity assessment
5.4.4 Mission conformance test
5.4.5 Charge and discharge test
26 5.4.6 Thermal vacuum test
5.4.7 Mechanical environment test
5.4.8 Cycle life test
5.4.9 Storage life test
6 Battery
6.1 Performance
6.1.1 General
6.1.2 C/n charge or discharge current (c-rate)[4][5][6]
6.1.3 Cut-off voltage
27 6.1.4 Cycle
6.1.5 Depth of discharge (DOD)[4][5][6][13]
6.1.6 End of charge voltage
6.1.7 Energy
6.1.8 Energy density
28 6.1.9 Energy reserve [4][5]
6.1.10 Fully charged [9][13]
6.1.11 Nameplate capacity
6.1.12 Nominal capacity
6.1.13 Nameplate energy [5][12]
6.1.14 Nominal voltage [9]
6.1.15 State of charge
29 6.1.16 Standard method for capacity measurement
6.1.17 Battery internal resistance (ohmic)
6.1.18 Battery impedance
6.1.19 Life test demonstration
30 6.1.20 For GEO simulated
6.1.21 For LEO simulated
6.1.22 For launch vehicle: simulate ground storage and usage at launch phase
6.1.23 Battery general requirements [5][11]
31 6.1.24 Electrical design
6.1.25 Thermal design
6.1.26 Mechanical design
6.1.27 Cell-to-cell balancing mechanisms
6.1.28 Marking
6.1.29 Cell matching
6.1.30 Polarization testing (optional)
32 6.1.31 Self-discharge rate test
6.1.32 Tailoring screening tests
6.1.33 Cell matching criteria
33 6.1.34 Contamination control
6.1.35 Test data trending [4]
6.1.36 Flight verification acceptance testing [5]
6.1.37 Assurance of the life estimation [8]
6.1.38 Parameter measurement tolerances
34 6.1.39 Battery testing [5][15]
6.1.40 Development testing [4][15]
6.1.41 Charge control testing
6.1.42 Thermal control testing
35 6.1.43 Mechanical test
6.1.44 Qualification test [4]
6.1.45 Qualification test levels and duration
6.1.46 In-process inspections and tests
6.1.47 Data collection and acquisition rates
36 6.2 Safety
6.2.1 General
37 6.2.2 Definitions of dangerous phenomenon
6.2.3 Technical requirement
6.2.4 Fault tolerance
38 6.2.5 Hazard controls [5]
6.2.6 Over-current prevention
6.2.7 Over-voltage protection
6.2.8 Temperature/current management
6.2.9 Insulation and wiring
39 6.2.10 Positive protection against accidental shorting
6.2.11 Venting
6.2.12 Crew touch temperature requirements
6.2.13 Terminal contacts
6.2.14 Safety testing
40 6.2.15 Important test considerations
41 6.2.16 Thermal runaway propagation
6.2.17 Special provision
6.2.18 Description for necessary information for system safety review
42 6.3 Logistics
6.3.1 General
6.3.2 Manufacture/assembly storage and testing
43 6.3.3 Safety measure for handling
6.3.4 Transportation
7 Battery onboard space vehicle
7.1 Performance
7.1.1 General
44 7.1.2 Basic design
7.1.3 Electrical ground bonding
7.1.4 Temperature reference point of battery module
7.1.5 Preparation for handling, transportation
45 7.2 Safety
7.2.1 General
7.2.2 Definitions of dangerous phenomenon
7.2.3 Technical requirement
7.3 Logistics
7.3.1 General
7.3.2 Safety measure for handling
46 7.3.3 Integration to the space vehicle
7.3.4 Battery maintenance on the space vehicle
7.3.5 Battery transportation equipped in space vehicle
47 8 Launch site
8.1 General
8.2 Performance
8.3 Safety
48 8.4 Logistics
8.4.1 General
8.4.2 Safety measure for handling
8.4.3 Preparation for transportation
8.4.4 SOC level for transportation
8.4.5 Container for transportation
8.4.6 Battery testing (health checking after transportation)
49 8.4.7 Inspection
8.4.8 State of health verification
8.4.9 Battery storage at launch site
8.4.10 Self-discharge rate
50 8.4.11 Protection under integration
8.4.12 Handling plate
8.4.13 Electrical connection
8.4.14 Electrical checkout
8.4.15 Battery monitoring
8.4.16 Battery monitoring preceding launch
9 Mission in orbit and end of life
52 Annex A (informative) Parameter measurement tolerances
53 Annex B (informative) Example of cell qualification test
55 Annex C (informative) Hazard identification method
57 Annex D (normative) Safety measure for handling
59 Annex E (informative) Transportation
63 Annex F (informative) Lot assessment of COTS cells
65 Bibliography

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BS ISO 17546:2024
$198.66