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Master Bond adhesives

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General Plastics LAST-A-FOAM® WSF-1121 Foam
Categories: Other Engineering Material; Composite Core Material; Polymer; Thermoset; Polyurethane, TS; Thermoset Polyurethane Foam, Unreinforced

Material Notes: LASTAFOAM WSF1121 (Impact Energy Absorption): These flame-retardant, durable, self-skinning foams (also referred to as integral-skin foams) are used extensively in aircraft flight decks and cabin applications. The harder, more durable of our flexible polyurethane foams, this tough integral-skin polyurethane foam system can be pigmented and in-mold painted for a lasting finish. WSF1121 products are used by airframe manufacturers for molded and fabricated flight-deck padding and aircraft interior parts. This self-extinguishing, flexible urethane foam can be custom-molded to your exacting specification. PLEASE NOTE: These foams are not offered for sale as liquid kits or sheet stock. They are only available within a finished parts program.

Advantages:

  • Durable
  • Flame-retardant
  • Self-skinning
  • Custom-molding ability
Applications
  • Flight-deck Padding
  • Flight-deck Parts
  • Passenger Cabin Walls and Ceilings
  • Passenger Compartment Overhead Stow Bins
  • Service-Class Divider Partitions
  • Food-Service Galleys
  • Lavatories
  • RTM/VARTM Core
  • Sub-munition Weapon Packaging
  • Prosthetic Limbs

Information provided by General Plastics Manufacturing Company

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Physical PropertiesOriginal ValueComments
Density 0.311 - 0.351 g/ccASTM D1622
 
Mechanical PropertiesOriginal ValueComments
Tensile Strength 132.5 psiASTM D3574, Test E
Elongation at Break 178 %ASTM D3574, Test E
Compressive Strength 60.3 psi
@Strain 50 %
Load Deflection; ASTM D3574, Test C
 60.6 psi
@Strain 50 %
Load Deflection, After Steam Autoclave Aging; ASTM D3574, Test C
 72.5 psi
@Strain 50 %
Load Deflection, After Dry Heat Aging,; ASTM D3574, Test C
Resilience 31.7ASTM D3574, Test H
Compression Set 8.1 %ASTM D3274, Test D
 
Descriptive Properties
Burn Length1.1 inAfter Steam Autoclave Aging
 1.7 in
 2 inAfter Dry Heat Aging
Extinguish Time1.7 secChapter 1 of FAA Aircraft Materials Fire Test Handbook
 4 secAfter Seat Autoclave Aging, Chapter 1 of FAA Aircraft Materials Fire Test Handbook
 9.2 secAfter Dry Heat Aging, Chapter 1 of FAA Aircraft Materials Fire Test Handbook
 No DripsAfter Dry Heat Aging, Drip Extinguish Time, Chapter 1 of FAA Aircraft Materials Fire Test Handbook
 No DripsAfter Seat Autoclave Aging, Drip Extinguish Time, Chapter 1 of FAA Aircraft Materials Fire Test Handbook
 No DripsDrip Extinguish Time, Chapter 1 of FAA Aircraft Materials Fire Test Handbook
Puncture Resistance4 kg(f)
 4 kg(f)After Dry Heat Aging,
 5 kg(f)After Steam Autoclave Aging

Some of the values displayed above may have been converted from their original units and/or rounded in order to display the information in a consistent format. Users requiring more precise data for scientific or engineering calculations can click on the property value to see the original value as well as raw conversions to equivalent units. We advise that you only use the original value or one of its raw conversions in your calculations to minimize rounding error. We also ask that you refer to MatWeb's terms of use regarding this information. Click here to go back to viewing the property data in MatWeb's normal format.

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PGENR086 / 186872

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