Lithium-ion Cell for Space Applications (JMG050)(50Ah)
50 Ah(JMG050)
| Registration date | 4/21/2008 (6/22/2011) |
|---|---|
| JAXA development group | Research Unit I, Research and Development Directorate |
| View diagram | See Attachment 1 |
| Environmental resistance | See Attachment 2 |
| Patent number (publication number) |
N/A |
| Reference | N/A |
| Satellite and launch date | To be supplied after launch |
| Note | N/A |
Manufacturer
GS Yuasa Technology Ltd.
Kyoto-shi, Kyoto, Japan
https://www.gs-yuasa.com/gyt/jp/
Features
The feature of the lithium ion Cell.
- High energy density
Less than 1/2 which is Ni-Cd battery compared with the mass. - No memory effect
No reconditioning is required on-orbit. - Small self-discharge
Reduce the launch operation for back-up charge of batteries.
Applications
Supply of electric power to a satellite/probe when solar power is not available (eclipse period).
Specifications
| Property | JMG050 | Remarks |
|---|---|---|
| Cell Configuration | Elliptic cylinder | - |
| Cathode | LiCoO2 | - |
| Anode | Graphite | - |
| Capacity | 50 Ah | Rated capacity |
| Average discharge voltage | 3.7 V | - |
| Weight | 1,510 g | - |
| Dimensions (W×D×H) | 130 mm × (52 mm) × 131 mm | Excluding stud bolt terminals |
| Energy density | 123 Wh/kg, 231 Wh/L | Values based on the rated capacity |
