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Safe, High Power / Voltage Battery Design ChallengesNASA seeks safe, high performing battery module designs that can deliver 3C discharge rates continuously, achieve 160 Wh/kg, and is passively propagation resistant to a single cell thermal runaway event. One solution is presented that uses a patented oscillating heat pipe technology for thermal management. Combined with light weight packaging and a new commercially available gas permeable vent port, all 5 preliminary safety tests results performed to date are showing ample margins.
Document ID
20200002348
Acquisition Source
Johnson Space Center
Document Type
Presentation
Authors
Darcy, Eric ORCID
(NASA Johnson Space Center Houston, TX, United States)
Darst, Jacob
(NASA Johnson Space Center Houston, TX, United States)
Walker, Will
(NASA Johnson Space Center Houston, TX, United States)
Yowtak, Kris
(NASA Johnson Space Center Houston, TX, United States)
Nunez, Jacob
(NASA Johnson Space Center Houston, TX, United States)
Rogers, Jim
(Jacobs Engineering Group Houston, TX, United States)
Tran, Minh N.
(CACI, Inc. Reston, VA, United States)
Russell, Sam
(NASA Johnson Space Center Houston, TX, United States)
Quinn, Alex
(NASA Johnson Space Center Houston, TX, United States)
Coman, Paul
(J.A. White & Associates Inc Columbia, SC, United States)
White, Ralph
(J.A. White & Associates Inc Columbia, SC, United States)
Bayles, Gary
(Science Applications International Corp. Greenbelt, MD, United States)
Strangways, Brad
(SRI International Corp. Birmingham, AL, United States)
Pounds, Den
(Thermavant Technologies, LLC Columbia, MO, United States)
Alexander, Ben
(Thermavant Technologies, LLC Columbia, MO, United States)
Mo, Michael
(KULR Technology Group San Diego, CA, United States)
Date Acquired
April 14, 2020
Publication Date
November 19, 2019
Subject Category
Electronics And Electrical Engineering
Report/Patent Number
JSC-E-DAA-TN75153
Meeting Information
Meeting: NASA Aerospace Battery Workshop
Location: Huntsville, AL
Country: United States
Start Date: November 19, 2019
End Date: November 21, 2019
Sponsors: NASA Marshall Space Flight Center
Funding Number(s)
TASK: NESC-TA-17-01912
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
High power
Thermal runaway
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