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Vehicle acceleration Documentation Polymers AMS P17 Polymer Matrix Composites Committee Technical review Transportation Systems

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Standard

265°F Vacuum Cure, Epoxy Prepregs
2017-11-08
WIP
AMS6566
The purpose of this specification is to allow procurement of a defined material corresponding to statistically derived material properties published in CMH-17. This material is intended for use in laminate applications with a service temperature up to 180 °F. They are typically used in structural applications requiring high strength and stiffness. This is the base specification and it will have one slash/detail specs.
Standard

265°F Vacuum Cure, Epoxy Prepregs Type 42, Class 2, Grade 193, Style 12K-193-SFP-OSI
2017-11-10
WIP
AMS6566/1
The purpose of this specification is to allow procurement of a defined material corresponding to statistically derived material properties published in CMH-17. This material is intended for use in laminate applications with a service temperature up to 180 °F. They are typically used in structural applications requiring high strength and stiffness. This is the base specification and it will have one slash/detail specs.
Standard

265°F, Autoclave Vacuum Bag Cure, Epoxy Prepreg, Type 33, Class 1, Grade 148, Intermediate Modulus Carbon Fiber
2017-11-10
WIP
AMS6568/1
The purpose of this specification is to allow procurement of a defined material corresponding to statistically derived material properties published in CMH-17. This material is intended for use in laminate applications with a service temperature up to 180 °F. They are typically used in structural applications requiring high strength and stiffness. This is the base specification and it will have three slash/detail specs.
Standard

265°F, Autoclave Vacuum Bag Cure, Epoxy Prepreg, Type 40, Class 2, Grade 195, Style 3K-PW, Standard Modulus Carbon Fiber
2017-11-10
WIP
AMS6568/2
The purpose of this specification is to allow procurement of a defined material corresponding to statistically derived material properties published in CMH-17. This material is intended for use in laminate applications with a service temperature up to 180 °F. They are typically used in structural applications requiring high strength and stiffness.
Standard

265°F, Autoclave Vacuum Bag Cure, Epoxy Prepregs
2017-11-08
WIP
AMS6568
The purpose of this specification is to allow procurement of a defined material corresponding to statistically derived material properties published in CMH-17. This material is intended for use in laminate applications with a service temperature up to 180 °F. They are typically used in structural applications requiring high strength and stiffness. This is the base specification and it will have three slash/detail specs.
Standard

Autoclave Cure, High Toughness and High Open-Hole Compression Epoxy Prepreg, Type 33, Class 1, Grade 190, Intermediate Modulus Carbon Fiber
2017-11-10
WIP
AMS6569/1
The purpose of this specification is to allow procurement of a defined material corresponding to statistically derived material properties published in CMH-17. These materials are designed specifically for vacuum bag autoclave cure. These materials are intended for use in laminate applications with a service temperature up to 180 °F. They are typically used in structural applications requiring high strength and stiffness.
Standard

Autoclave Cure, High Toughness and High Open-Hole Compression Epoxy Prepreg, Type 38, Class 2, Grade 193, Style 3K-PW, Standard Modulus Carbon Fiber
2017-11-10
WIP
AMS6569/2
The purpose of this specification is to allow procurement of a defined material corresponding to statistically derived material properties published in CMH-17. These materials are designed specifically for vacuum bag autoclave cure. These materials are intended for use in laminate applications with a service temperature up to 180 °F. They are typically used in structural applications requiring high strength and stiffness.
Standard

Autoclave Cure, High Toughness and High Open-Hole Compression Epoxy Prepregs
2017-11-08
WIP
AMS6569
The purpose of this specification is to allow procurement of a defined material corresponding to statistically derived material properties published in CMH-17. These materials are designed specifically for vacuum bag autoclave cure. These materials are intended for use in laminate applications with a service temperature up to 180 °F. They are typically used in structural applications requiring high strength and stiffness. This is the base specification and it will have two slash/detail specs.
Standard

Boron Filament Tape, Epoxy-Resin-Impregnated
2016-10-12
CURRENT
AMS3867C
This specification and its supplementary detail specifications cover boron filaments in the form of tape impregnated with epoxy resin, the resin to be supplied in a “B” stage condition.
Standard

Boron Filament Tape, Epoxy-Resin-Impregnated
2001-04-01
HISTORICAL
AMS3867B
This specification and its supplementary detail specifications cover boron filaments in the form of tape impregnated with epoxy resin, the resin to be supplied in a “B” stage condition.
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