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Tow, Carbon Fiber For Structural Composites 550 (3792) Tensile Strength, 38 (262) Tensile Modulus

AMS P17 Polymer Matrix Composites Committee
  • Aerospace Material Specification
  • AMS3892/10B
  • Current
Published 2016-12-27 by SAE International in United States
This specification covers one type of carbon fiber in the form of tow.
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Tow or Yarn, Carbon Fibers For Structural Composites GF 400 (2758) Tensile Strength, 40 (276) Tensile Modulus

AMS P17 Polymer Matrix Composites Committee
  • Aerospace Material Specification
  • AMS3892/3C
  • Current
Published 2016-12-16 by SAE International in United States
This specification covers one type of continuous multifilament carbon fibers in the form of a tow or yarn (when twisted). The weight per unit length of the tow or yarn is governed by the filament count which is identified by the supplier's grade or material designation.
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Tow or Yarn, Carbon Fibers For Structural Composites GF 400 (2758) Tensile Strength, 33 (228) Tensile Modulus

AMS P17 Polymer Matrix Composites Committee
  • Aerospace Material Specification
  • AMS3892/1C
  • Current
Published 2016-12-16 by SAE International in United States
This specification covers one type of continuous multifilament carbon fibers in the form of a tow or yarn (when twisted). The weight per unit length of the tow or yarn is governed by the filament count which is identified by the supplier's grade or material designation.
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Roving, Type "S-2" Glass Epoxy Resin Impregnated

AMS P17 Polymer Matrix Composites Committee
  • Aerospace Material Specification
  • AMS3832D
  • Current
Published 2016-12-16 by SAE International in United States
This specification covers continuous, multiple-strand, roving of Type "S-2" glass impregnated with a heat-curable epoxy resin matrix and processed to a "B" stage condition.
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Tow or Yarn, Carbon Fibers For Structural Composites GF 220 (1517) Tensile Strength, 75 (517) Tensile Modulus

AMS P17 Polymer Matrix Composites Committee
  • Aerospace Material Specification
  • AMS3892/5C
  • Current
Published 2016-12-16 by SAE International in United States
This specification covers one type of continuous multifilament carbon fibers in the form of a tow or yarn (when twisted). The weight per unit length of the tow or yarn is governed by the filament count which is identified by the supplier's grade or material designation.
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Tow or Yarn, Carbon Fibers For Structural Composites GF 325 (2241) Tensile Strength, 57 (393) Tensile Modulus

AMS P17 Polymer Matrix Composites Committee
  • Aerospace Material Specification
  • AMS3892/6B
  • Current
Published 2016-12-16 by SAE International in United States
This specification covers one type of continuous multifilament carbon fibers in the form of a tow or yarn (when twisted). The weight per unit length of the tow or yarn is governed by the filament count which is identified by the supplier's grade or material designation.
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Cloth, Type "E" Glass, Style 7781 Fabric Hot-Melt, Addition-Type, Polyimide Resin Impregnated

AMS P17 Polymer Matrix Composites Committee
  • Aerospace Material Specification
  • AMS3844C
  • Current
Published 2016-12-16 by SAE International in United States
This specification covers one type of glass cloth impregnated with a heat-reactive, thermosetting, hot-melt, addition-type, polyimide resin system, furnished in continuous rolls of full width material.
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Fibers, Carbon, Tow and Yarn For Structural Composites

AMS P17 Polymer Matrix Composites Committee
  • Aerospace Material Specification
  • AMS3892C
  • Current
Published 2016-12-15 by SAE International in United States
This specification and its supplementary detail specifications cover carbon fibers in the form of continuous multifilament tow and yarn.
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Cloth, Type “E” Glass, “B” Stage Polyester-Resin-Impregnated 7781 Style Fabric, Flame Resistant, Improved Strength

AMS P17 Polymer Matrix Composites Committee
  • Aerospace Material Specification
  • AMS3834B
  • Current
Published 2016-12-15 by SAE International in United States
This specification covers a style 7781 glass cloth impregnated with a heat-curable polyester resin system, the resin being processed to a “B” stage condition, and furnished in the form of continuous rolls.
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Graphite Yarn, Non-Structural 5 Ply Yarn, 720 Filaments

AMS P17 Polymer Matrix Composites Committee
  • Aerospace Material Specification
  • AMS3890B
  • Current
Published 2016-12-15 by SAE International in United States
The product shall consist of 5-ply yarn having 720 continuous filaments per ply and a maximum of 4 turns per inch (25.4 mm).
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