GB/T 42635-2023 (GB/T42635-2023, GBT 42635-2023, GBT42635-2023) & related versions
| Standard ID | Contents [version] | USD | STEP2 | [PDF] delivered in | Standard Title (Description) | See Detail | Status | Similar PDF |
| GB/T 42635-2023 | English | 350 |
Add to Cart
|
0-9 seconds. Auto delivery.
|
General specification of lithium-ion cells for aerospace
|
GB/T 42635-2023
| Valid |
GBT 42635-2023
|
Buy with any currencies (Euro, JPY, KRW...): GB/T 42635-2023 Preview this PDF: GB/T 42635-2023
GB/T 42635-2023
GB
NATIONAL STANDARD OF THE
PEOPLE’S REPUBLIC OF CHINA
ICS 29.220.01
CCS K 82
General specification of lithium-ion cells for aerospace
ISSUED ON: MAY 23, 2023
IMPLEMENTED ON: SEPTEMBER 01, 2023
Issued by: State Administration for Market Regulation;
Standardization Administration of the People's Republic of China.
Table of Contents
Foreword ... 4
1 Scope ... 5
2 Normative references ... 5
3 Terms and definitions ... 5
4 Symbols and abbreviations ... 6
5 Requirements ... 6
5.1 General ... 6
5.2 Appearance and marks ... 7
5.3 Dimensions and quality ... 7
5.4 Sealing ... 7
5.5 Electrical properties ... 7
5.6 Environmental adaptability ... 8
5.7 Safety performance ... 8
5.8 Cycling life ... 9
5.9 Irradiation ... 9
6 Test methods ... 9
6.1 Test conditions ... 9
6.2 Appearance and marks ... 10
6.3 Dimensions and quality ... 10
Figure 1 -- Schematic diagram of cell appearance ... 11
6.4 Sealing ... 11
6.5 Electrical properties ... 11
Figure 2 -- Schematic diagram of DC internal resistance discharge ... 13
Figure 3 -- Schematic diagram of pulse discharge ... 14
6.6 Environmental adaptability ... 14
Figure 4 -- Schematic diagram of cell coordinates ... 15
Table 1 -- Random vibration test conditions ... 15
Table 2 -- Sinusoidal vibration test conditions ... 16
Table 3 -- Impact test conditions (impact response spectrum ... 16
Figure 5 -- Thermal vacuum test cycle diagram ... 17
Table 4 -- Thermal vacuum test conditions ... 17
6.7 Safety performance ... 17
6.8 Cycling life ... 19
Table 5 -- Shadow period and discharge time for geostationary orbit (GEO) cycling test
... 21
6.9 Irradiation ... 21
Figure 6 -- Schematic diagram for the direction of the irradiation test ... 22
Table 6 -- Charged particle irradiation test conditions ... 22
7 Inspection rules ... 22
7.1 Inspection classification ... 22
7.2 Appraisal inspection ... 23
Table 7 -- Appraisal inspection items, grouping and sequence ... 23
7.3 Quality consistency inspection ... 24
8 Packaging, transportation and storage ... 25
8.1 Packaging ... 25
8.2 Transportation ... 25
8.3 Storage ... 25
General specification of lithium-ion cells for aerospace
1 Scope
This document specifies the technical requirements, test methods, inspection rules,
packaging, transportation and storage of lithium-ion cells for aerospace (hereinafter
referred to as "cell").
This document applies to lithium-ion cells for space vehicles such as satellites, space
stations, and space probes.
2 Normative references
The following referenced documents are indispensable for the application of this
document. For dated references, only the edition cited applies. For undated references,
the latest edition of the referenced document (including any amendments) applies.
GB/T 191, Packaging and storage marks
GB/T 2900.41, Electrotechnical terminology -- Primary and secondary cells and
batteries
3 Terms and definitions
For the purposes of this document, the terms and definitions defined in GB/T 2900.41
as well as the followings apply.
3.1 Coulomb efficiency
The ratio of the capacity output when the cell is discharged to the capacity input during
previous charging.
3.2 energy efficiency
The ratio of the energy output when a cell is being discharged to the energy input when
it was previously charged.
[Source: GB/T 2900.41-2008, 482-05-53]
3.3 cycling
A group of operations that are regularly repeated on the cell in the same sequence.
The high temperature capacity of the cell shall not be less than 95% of the rated capacity.
5.5.7 Low temperature capacity
The low temperature capacity of the cell shall not be less than 80% of the rated capacity.
5.5.8 Pulse test
The voltage during the cell pulse test shall not be lower than 3.3 V or the value specified
in the product technical conditions provided by the manufacturer.
5.6 Environmental adaptability
5.6.1 Steady-state acceleration
When the cell is tested according to 6.6.1, the discharge current and discharge voltage
shall have no sudden changes and no mechanical damage.
5.6.2 Random vibration
When the cell is tested according to 6.6.2, the discharge current and discharge voltage
shall have no sudden changes and no mechanical damage.
5.6.3 Sinusoidal vibration
When the cell is tested according to 6.6.3, the discharge current and discharge voltage
shall have no sudden changes and no mechanical damage.
5.6.4 Impact
When the cell is tested according to 6.6.4, the discharge current and discharge voltage
shall have no sudden changes and no mechanical damage.
5.6.5 Thermal vacuum
When the cell is tested according to 6.6.5, it shall not deform, crack or leak.
5.7 Safety performance
5.7.1 Short circuit
When the cell is tested according to 6.7.1, it shall not catch fire or explode.
5.7.2 Overcharging
When the cell is tested according to 6.7.2, it shall not catch fire or explode.
5.7.3 Over-discharging
When the cell is tested according to 6.7.3, it shall not catch fire or explode.
5.7.4 Overtemperature
When the cell is tested according to 6.7.4, it shall not catch fire or explode.
5.8 Cycling life
5.8.1 Low Earth Orbit (LEO) cycling life performance
For cells used in Low Earth Orbit, the number of cycles shall reach 48,000 times at 20%
DOD. The number of life assessments submitted for identification shall comply with
the requirements of the product technical conditions provided by the manufacturer.
5.8.2 Geosynchronous orbit (GEO) cycling life performance
The number of cycles of cells used in geosynchronous orbit shall reach 2,000 times.
The number of life assessments submitted for identification shall comply with the
requirements of the product technical conditions provided by the manufacturer.
5.9 Irradiation
When the cell is tested according to 6.9, it shall be well sealed and not bulge.
6 Test methods
6.1 Test conditions
6.1.1 Environmental conditions
Unless otherwise specified, each test shall be conducted under the following
environmental conditions:
a) Temperature: 15℃~35℃;
b) Relative humidity: 20%~80%;
c) Air pressure: 86 kPa ~ 106 kPa.
6.1.2 Measuring instruments and instrument requirements
The requirements for measuring instruments and meters are:
a) The accuracy of dimensional measurement tools shall not be less than 0.02 mm.
b) The sensing capacity of the electronic balance shall not be less than 0.00 1kg.
6.7.2 Overcharging
Carry out the overcharge test according to the following steps:
a) Stabilize the cell temperature at 20℃±3℃;
b) Charge to 4.5 V at 0.1 C1A or the value specified in the product technical
conditions provided by the manufacturer;
c) Let it stand for 60 min ~ 75 min;
d) Discharge to 2.75 V at 0.67 C1A or the value specified in the product technical
conditions provided by the manufacturer;
e) Repeat steps a) ~ d) for a total of 10 times.
6.7.3 Over-discharging
Carry out over-discharging test according to the following steps:
a) Stabilize the cell temperature at 20℃±3℃;
b) Charge to 4.1 V at 0.1 C1A or the value specified in the product technical
conditions provided by the manufacturer;
c) Charge at constant voltage until the current drops to 0.05 C1A;
d) Let it stand for 60 min ~ 75 min;
e) Discharge to 2.75 V with a current of 0.67 C1A;
f) Continue to discharge at a current of 0.67 C1A to -0.8 V or 1.2 h, whichever comes
first, or in accordance with the product technical conditions provided by the
manufacturer;
g) Repeat steps a) ~ f) for a total of 10 times.
6.7.4 Overtemperature
In an environment of 20℃±3℃, discharge the cell at a constant current of 0.2 C1A to
2.75 V or the value specified by the product technical conditions provided by the
manufacturer. Place the cell in a constant temperature box at 60℃±2℃. Carry out over-
temperature test as follows:
a) Let stand for 24 h;
b) Charge to 4.1 V at 0.2 C1A or the value specified by the product technical
conditions provided by the manufacturer;
c) Charge at constant voltage until the current drops to 0.05 C1A;
d) Let it stand for 10 min;
e) Discharge at 0.2 C1A constant current to 2.75 V or the value specified in the
product technical conditions provided by the manufacturer.
6.8 Cycling life
6.8.1 Low Earth Orbit (LEO) cycling life performance
The cell low earth orbit (LEO) cycling life test shall be performed in accordance with
the product technical conditions provided by the manufacturer. If there is no provision,
the following provisions may apply.
a) In an environment of 20°C± 3°C, charge the cell with a constant current of 0.2
C1A to 3.95 V or the value specified in the product technical conditions provided
by the manufacturer. When the charging current drops to 0.01 C1A, the charging
ends. After leaving it alone for 1 h, conduct cycling through the following steps:
1) Discharge the cell at a current of 0.4 C1A for 30 min;
2) Charge at 0.3 C1A constant current to 3.95 V or convert to constant voltage
charging according to the product technical conditions provided by the
manufacturer. Charging ends when the charging current drops to 0.01 C1A or
the charging time reaches 60 min;
3) Repeat 1) and 2) charge and discharge cycles. Record the discharge termination
voltage for each charge-discharge cycle.
b) During the cycle, when the discharge end voltage of three consecutive cycles is
lower than 3.30 V or the value specified in the product technical conditions
provided by the manufacturer, the constant current charge cutoff voltage is
increased in steps of 0.05 V. After the charge cut-off voltage is raised to 4.1 V or
the value specified in the product technical conditions provided by the
manufacturer, if the discharge end voltage for 5 consecutive cycles is lower than
2.75 V or the specified value in the product technical conditions provided by the
manufacturer, the test ends. The accumulated number of cycles at this time shall
be the cycling life.
6.8.2 Geosynchronous orbit (GEO) cycling life performance
The cell geostationary orbit (GEO) cycling life test shall be performed in accordance
with the product technical conditions provided by the manufacturer. If there is no
provision, the following provisions may apply.
a) In an environment of 20℃±3℃, the cell shall be cycled according to the following
steps:
1) The cell is charged to 4.0 V at a constant current of 0.2 C1A or to constant
voltage charging according to the product technical conditions provided by the
manufacturer;
2) Charging ends when the charging current drops to 0.01 C1A. After standing for
0.5 h ~ 1 h, discharge with a current of 0.67 C1A according to the weekly
discharge time shown in Table 5 (for example, the first weekly discharge is
21.00 min);
3) Then charge in the same way. After charging is completed and left to stand for
0.5 h ~ 1 h, discharge is performed with a current of 0.67 C1A according to the
weekly discharge time shown in Table 5 (for example, the second weekly
discharge is 29.37 min). By analogy, one week is one cycle. In 1 shadow period,
conduct 45 charge and discharge cycles;
4) Charge the cell with a constant current of 0.2 C1A to 4.0 V or the value specified
in the product technical conditions provided by the manufacturer. Switch to
constant voltage charging. Charging ends when the charging current drops to
0.01 C1A. Fully charge and left for 10 d. Enter the second shadow period;
5) Repeat 1) ~ 4) charge and discharge cycle. Record the discharge termination
voltage for each cycle.
b) When the final discharge voltage of the cell for three consecutive cycles during a
certain shadow period is lower than 3.0 V or the value specified by the product
technical conditions provided by the manufacturer, the charge cut-off voltage is
increased in steps of 0.05 V. After the charging cut-off voltage is adjusted to 4.1
V or the value specified in the product technical conditions provided by the
manufacturer, if the final discharge voltage for 5 consecutive cycles is lower than
2.75 V or the specified value in the product technical conditions provided by the
manufacturer, the test shall end. The accumulated number of cycles at this time
shall be the cycling life.
The inspection items, technical requirements, inspection methods and inspection
sequences of Group B shall be carried out in accordance with the provisions of Table 7.
For Group B inspection, randomly select 4 products from Group A inspection. After the
four cells have completed high-temperature capacity, low-temperature capacity, pulse
test, steady-state acceleration, random vibration, sinusoidal vibration, impact, thermal
vacuum and other inspection items, one of each of the four cells will be selected for
short circuit, overcharge, over-discharge, over-discharge and over temperature
inspection.
The inspection cycle is 2 years.
8 Packaging, transportation and storage
8.1 Packaging
Cells shall be packed with moisture-proof materials. Shock absorption and insulation
measures shall be taken for packing.
The marks on the packaging box shall comply with GB/T 191 and the following
regulations:
a) The content of the mark shall include product model and batch number;
b) The packaging box shall have the manufacturer’s logo.
8.2 Transportation
During transportation, the state of charge of the cell shall be between 40% and 60%.
Cells can be transported by road, railway, etc. The maximum mechanical magnitude
experienced by the cell during transportation shall be lower than the magnitudes in 6.6.1,
6.6.2, 6.6.3, and 6.6.4.
The ambient temperature of the cell during transportation is generally maintained at -
5℃ ~ +30℃. When the temperature exceeds 30℃, the transportation time shall be less
than 10 d. The time at this high temperature shall not exceed 4 h a day.
Temperature, humidity and abnormal mechanical magnitudes shall be recorded during
transportation.
8.3 Storage
When storing cells, the state of charge of the cell shall be between 40% and 60%.
......
| Standard ID | GB/T 42635-2023 (GB/T42635-2023) | | Description (Translated English) | General specification of lithium-ion cells for aerospace | | Sector / Industry | National Standard (Recommended) | | Classification of Chinese Standard | K82 | | Classification of International Standard | 29.220.01 | | Word Count Estimation | 20,218 | | Date of Issue | 2023-05-23 | | Date of Implementation | 2023-09-01 | | Drafting Organization | Shanghai Space Power Research Institute | | Administrative Organization | National Aerospace Technology and Its Application Standardization Technical Committee (SAC/TC 425) | | Proposing organization | National Aerospace Technology and Its Application Standardization Technical Committee (SAC/TC 425) | | Issuing agency(ies) | State Administration for Market Regulation, National Standardization Management Committee |
|