Battery Passivation
Programme Reference
T703-404EP
Status
Closed
Country
France
Start Date
2015
End Date
2018
Programme: TDE Prime Contractor: AIRBUS DEFENCE & SPACE SAS
Subcontractors:
ABSL SPACE PRODUCTS • United Kingdom
LETI • France
SAFT S.A.S • France
Objectives
Test Li-Ion battery cells under abuse and extreme conditions encountered after spacecraft disposal in order to assess their safety.
Description
At the end of its operational life a spacecraft undergoes a disposal phase and as a result is left without control. Then the battery may be subject to extreme environmental conditions due to the loss of spacecraft attitude and thermal control. Battery overdischarge or overcharge may also occur. Further battery cells get more and more aged and are then weakened.The goal is to test aged battery cells under various abuse conditions (overdischarge, overcharge, damaged) and different temperatures (hot, cold) in order to check their behaviour and assess their level of safety.This will provide an essential input to define the most adequate means to passivate the battery.
• Application domain: Generic Technologies
•
Technology Domain:
3 - Space Systems Electrical Power
3 - Space Systems Electrical Power
•
Competence Domain:
4-Electric Architecture, Power and Energy, EMC
4-Electric Architecture, Power and Energy, EMC
• Initial TRL: TRL 1
• Target TRL: TRL 3
• Achieved TRL: TRL 3
•HarmoRoadMap: N/A
•IPC Document: ESA/IPC(2014)3,add.6
•Public Document: