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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
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
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