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 PowerElectronics And Electrical Engineering