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Safe, High Power/Voltage Battery Module Design ChallengesNASA seeks to demonstrate a path for achieving safe, high power, and high performing Li-ion battery designs for the purpose of establishing design guidelines for our aeronautic and spacecraft applications. Safe means passively resistant to thermal runaway propagation of any single cell catastrophic thermal runaway. High power means capable of 3C continuous discharge without overheating. High performing means achieving > 160 Wh/kg, 200 Wh/L. The biggest challenge has been balancing a high flux light weight path for cell heat dissipation during the high rate discharge that minimizes thermal gradients between cells and also protects adjacent cells from the heat load of thermal runaway cell. Our solution includes an oscillating heat pipe spine that contacts every 18650 cell in the pack and careful cell design selection to maximize the range of initial temperatures conditions where the battery can safely complete the 3C discharge.
Document ID
20190014045
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)
Nogrady, Sean
(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)
Date Acquired
May 9, 2019
Publication Date
May 7, 2019
Subject Category
Electronics And Electrical Engineering
Report/Patent Number
JSC-E-DAA-TN73954
JSC-E-DAA-TN73384
JSC-E-DAA-TN66829
Meeting Information
Meeting: More Electric Aircraft Europe
Location: Hamburg
Country: Germany
Start Date: October 28, 2019
End Date: October 31, 2019
Sponsors: Cambridge Innovation Institute, International Quality and Productivity Center (IQPC)
Funding Number(s)
WBS: 869021.05.05.02.19
CONTRACT_GRANT: PC11708979
CONTRACT_GRANT: NNJ14HA04B
CONTRACT_GRANT: NNJ13HA01C
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
Single Expert
Keywords
Thermal runaway
High power
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