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Advanced Terminal Design for Prismatic Li-Ion Cell Eric Quee, EaglePicher Technologies Mike Pollack and Rich DiDomizio, EnvirOptics, Inc. 2015 NASA Aerospace Battery Workshop November 17-19, 2015 Huntsville, Alabama

Advanced Terminal Design for Prismatic Li-Ion Cell

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Advanced Terminal Design for Prismatic Li-Ion Cell

Eric Quee, EaglePicher Technologies

Mike Pollack and Rich DiDomizio, EnvirOptics, Inc.

2015 NASA Aerospace Battery Workshop November 17-19, 2015

Huntsville, Alabama

2 Copyright© 2015 EaglePicher Technologies, LLC

Outline

•  Existing Terminal Design Issues •  Advanced Terminal Design Objectives •  Qualification Test Plan and Initial Results •  Summary

3 Copyright© 2015 EaglePicher Technologies, LLC

Existing Terminal Design

•  Spade type terminal •  Positive Terminal 1100 Aluminum with Nickel plating •  Negative Terminal 101 Copper with Gold plating •  Terminal through hole bolt torqued to 20 in-lb •  Positive terminal known to relax under compression

–  Reduced terminal to lead contact force –  Increased resistance at the terminal interface

Terminal Tightened

4 Copyright© 2015 EaglePicher Technologies, LLC

Advanced Terminal Design •  Design Objectives

–  Provide robust electrical connection, not through threads –  Torque to 40 in-lb without backup nut –  Capable of resisting 60 in-lb of torque without movement

or loss of hermetic seal –  Mechanically stable over mission life, up to 15 years –  Fit in Gen 1.1 cell format –  Applicable for both positive and negative terminals

•  Design Features –  3/8-24 UNF 2A male thread 1.0” long –  0.600 diameter shoulder for direct electrical contact with

lugs –  Seal leak rate < 1.0 x 10-8 atm-cc/sec

–  Maintain hermetic seal at -40 to +75°C –  Terminal resistance less than 30 µΩ –  Nickel plating on both terminals

5 Copyright© 2015 EaglePicher Technologies, LLC

Qualification Test Plan •  Three separate tests

–  Initial baseline •  Insulation resistance •  Leak rate •  Resistance •  Torque resistance •  Tensile strength

–  Normal qualification •  -40 to +75°C, 6 hour dwells, leak test at temperature, two cycles •  CW torque after temperature exposure •  CW torque to failure

–  Accelerated life testing – 35 Amp current flow reversed daily •  0 to 75°C at > 80% RH, 11 hour dwells, 10 cycles

–  Accelerated ground storage •  5 to 75°C at > 80% RH, 15 minute dwells, 1020 cycles

–  Accelerated ground integration, testing •  -40 to 75°C no measurable humidity, 15 minute dwells, 756 cycles

–  Accelerated LEO mission

6 Copyright© 2015 EaglePicher Technologies, LLC

Test Flowchart Summary

7 Copyright© 2015 EaglePicher Technologies, LLC

Initial Testing and Normal Qualification Flowchart

Initial Testing for all Seals and Terminals

Destructive Lot Acceptance Testing Specified by EPT on each production order

8 Copyright© 2015 EaglePicher Technologies, LLC

Accelerated Life Test Summary

9 Copyright© 2015 EaglePicher Technologies, LLC

Accelerated Life Test Detail

10 Copyright© 2015 EaglePicher Technologies, LLC

Accelerated Life Test - Terminals

11 Copyright© 2015 EaglePicher Technologies, LLC

Accelerated Life Test - Controls

12 Copyright© 2015 EaglePicher Technologies, LLC

Test Results to Date

•  Tensile Test – Terminal only Sy = 25,300 psi

•  Torque Test – Terminal only No deformation at 65 in-lb torque

•  Bend Test – Terminal only Failure at 95 in-lb

•  Terminal Resistance –  13 samples tested –  Resistance measured between a

fixed length of 0.870 “ –  Resistance measured at 0° and 90°

rotated then averaged –  Resistance range 10.3 to 10.65 µΩ

13 Copyright© 2015 EaglePicher Technologies, LLC

Summary

•  New positive terminal has been designed to address material relaxation

•  Terminal assemblies are being tested including –  Initial characterization –  Normal qualification testing –  Accelerated life testing

•  Accelerated life testing to simulate on ground and LEO mission requirements

•  Initial results are positive

14 Copyright© 2015 EaglePicher Technologies, LLC

Thank You