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International Space Station Lithium-Ion Battery Start-Up and CyclingThe International Space Station (ISS) primary Electric Power System (EPS) was originally designed to use Nickel-Hydrogen (Ni-H2) batteries to store electrical energy. The electricity for the ISS is generated by its solar arrays, which charge batteries during insolation for subsequent discharge during eclipse. The Ni-H2 batteries were designed to operate at a 35 depth of discharge (DOD) maximum during normal operation in a Low Earth Orbit. In 2010, the ISS Program began the development of Lithium-Ion (Li-Ion) batteries to replace Ni-H2 batteries approaching the end of their useful life and concurrently funded a Li-Ion ORU (Orbital Replacement Unit) and cell life testing project. The first set of 6 Li-ion battery replacements was launched in December 2016 and deployed in January 2017. This paper will discuss the Li-ion battery on-orbit cycling and the status of the Li-Ion cell and ORU life cycle testing.
Document ID
20180003481
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Dalton, Penni J.
(NASA Glenn Research Center Cleveland, OH, United States)
Bowens, Ebony
(Boeing Co. Houston, TX, United States)
North, Timothy R.
(Boeing Co. Houston, TX, United States)
Balcer, Sonia
(Aerojet Rocketdyne, Inc. Huntsville, AL, United States)
Date Acquired
June 6, 2018
Publication Date
November 14, 2017
Subject Category
Spacecraft Propulsion And Power
Electronics And Electrical Engineering
Report/Patent Number
GRC-E-DAA-TN48106
Report Number: GRC-E-DAA-TN48106
Meeting Information
Meeting: NASA Aerospace Battery Workshop
Location: Huntsville, AL
Country: United States
Start Date: November 14, 2017
End Date: November 16, 2017
Sponsors: NASA Marshall Space Flight Center
Funding Number(s)
CONTRACT_GRANT: NAS15-1000
WBS: WBS 401769.06.01.01.06
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
International Space Station
Lithium-Ion
Battery
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