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BS ISO 17546:2024 – TC

BS ISO 17546:2024 – TC

$258.95

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

Published By Publication Date Number of Pages
BSI 2024 167
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PDF Catalog

PDF Pages PDF Title
102 undefined
108 Foreword
109 Introduction
111 1 Scope
2 Normative references
3 Terms and definitions
116 4 Symbols and abbreviated terms
5 Cell
5.1 Performance
5.1.1 General
117 5.1.2 Test requirements
5.1.3 Test data trending [4]
118 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
119 5.1.9 Radiation test
5.1.10 Life cycle test
120 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
121 5.2.4 Safety testing
122 5.2.5 Important test considerations
123 5.2.6 Optional test
5.3 Logistics
5.3.1 General
124 5.3.2 Cell manufacturing, storage and testing
5.3.3 Safety measure for handling
125 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
126 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
127 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
128 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
129 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
130 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]
131 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)
132 6.1.31 Self-discharge rate test
6.1.32 Tailoring screening tests
6.1.33 Cell matching criteria
133 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
134 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
135 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
136 6.2 Safety
6.2.1 General
137 6.2.2 Definitions of dangerous phenomenon
6.2.3 Technical requirement
6.2.4 Fault tolerance
138 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
139 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
140 6.2.15 Important test considerations
141 6.2.16 Thermal runaway propagation
6.2.17 Special provision
6.2.18 Description for necessary information for system safety review
142 6.3 Logistics
6.3.1 General
6.3.2 Manufacture/assembly storage and testing
143 6.3.3 Safety measure for handling
6.3.4 Transportation
7 Battery onboard space vehicle
7.1 Performance
7.1.1 General
144 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
145 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
146 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
147 8 Launch site
8.1 General
8.2 Performance
8.3 Safety
148 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)
149 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
150 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
152 Annex A (informative) Parameter measurement tolerances
153 Annex B (informative) Example of cell qualification test
155 Annex C (informative) Hazard identification method
157 Annex D (normative) Safety measure for handling
159 Annex E (informative) Transportation
163 Annex F (informative) Lot assessment of COTS cells
165 Bibliography

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BS ISO 17546:2024 - TC
$258.95