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Peel Adhesion Test for Glass to Elastomeric Material for Automotive Glass Encapsulation

  • Ground Vehicle Standard
  • J1907_202101
  • Current
Published 2021-01-07 by SAE International in United States
Annotation ability available
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Overlap Shear Test for Sealant Adhesive Bonding of Automotive Glass Encapsulating Material to Body Opening

  • Ground Vehicle Standard
  • J1836_202101
  • Current
Published 2021-01-07 by SAE International in United States
Annotation ability available
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Overlap Shear Test for Automotive Type Sealant for Stationary Glass Bonding

  • Ground Vehicle Standard
  • J1529_202101
  • Current
Published 2021-01-07 by SAE International in United States
Annotation ability available
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Coach Joint Fracture Test

  • Ground Vehicle Standard
  • J1863_202101
  • Current
Published 2021-01-07 by SAE International in United States
Annotation ability available
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Metal to Metal Overlap Shear Strength Test for Automotive Type Adhesives

  • Ground Vehicle Standard
  • J1523_202101
  • Current
Published 2021-01-07 by SAE International in United States
This content contains downloadable datasets
Annotation ability available
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Carbon Fiber and Fiberglass Epoxy/Prepreg Products with 350 °F (177 °C) Cure for Aerospace Applications: Type 40, Class 1, Grade 196, Style 6K-PW

  • Aerospace Material Specification
  • AMS6891/2
  • Current
Published 2020-12-29 by SAE International in United States
This content contains downloadable datasets
Annotation ability available
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Carbon Fiber and Fiberglass Epoxy Prepreg Products with 350 °F (177 °C) Cure for Aerospace Applications: Type 35, Class 1, Grade 191

  • Aerospace Material Specification
  • AMS6891/1
  • Current
Published 2020-12-29 by SAE International in United States
This content contains downloadable datasets
Annotation ability available
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Intrusion Resistance of Safety Glazing Systems for Road Vehicles

  • Ground Vehicle Standard
  • J2568_202010
  • Current
Published 2020-10-19 by SAE International in United States
This content contains downloadable datasets
Annotation ability available
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Unidirectional Carbon Fiber Tape Epoxy Repair Prepreg, Vacuum Curing Part 5 - Material Specification for Unidirectional Carbon Fiber Tape Epoxy Prepreg for Repair and Film Adhesive for Repair, 120 to 145 °C (250 to 290 °F) Curing

  • Aerospace Material Specification
  • AMS6885/5
  • Current
Published 2021-02-22 by SAE International in United States
This content contains downloadable datasets
Annotation ability available
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new

Light Transmitting Glass Covers for Exterior Aircraft Lighting

  • Aerospace Standard
  • AIR5689B
  • Current
Published 2021-05-13 by SAE International in United States
This content contains downloadable datasets
Annotation ability available