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2014-08-26
WIP Standard
P1713AI/1
Detail specification for T700S-12K-50C/#2511 Plain Weave Fabric
2014-08-06
WIP Standard
AMS3904C
This specification and its supplementary detail specifications cover intermediate modulus papa-aramid fibers in the form of continuous, multifilament yarn and roving. These products have been used typically as primary elements in cables, cordage, and woven goods, but usage is not limited to such applications. Each application should be considered individually.
2014-08-06
WIP Standard
AMS3904/9B
This specification covers one type of organic (para-aramid) fiber in the form of yarn. The product shall be formed as a multiplicity of filaments drawn together and gathered into an approximately parallel arrangement.
2014-08-06
WIP Standard
AMS3904/7B
This specification covers one type of organic (para-aramid) fiber in the form of yarn. The product shall be formed as a multiplicity of filaments drawn together and gathered into an approximately parallel arrangement.
2014-08-06
WIP Standard
AMS3904/6B
This specification covers one type of organic fiber in the form of yarn. The product shall be formed as a multiplicity of filaments drawn together and gathered into an approximately parallel arrangement.
2014-08-06
WIP Standard
AMS3904/5C
This specification covers one type of organic (para-aramid) fiber in the form of yarn. The product shall be formed as a multiplicity of filaments drawn together and gathered into an approximately parallel arrangement.
2014-08-06
WIP Standard
AMS3904/2C
This specification covers one type of organic (para-aramid) fiber in the form of yarn. The product shall be formed as a multiplicity of filaments drawn together and gathered into an approximately parallel arrangement.
2014-08-06
WIP Standard
AMS3904/3C
This specification covers one type of organic (para-aramid) fiber in the form of yarn. The product shall be formed as a multiplicity of filaments drawn together and gathered into an approximately parallel arrangement.
2014-08-06
WIP Standard
AMS3904/11B
This specification covers one type of organic (para-aramid) fiber in the form of roving. The product shall be formed as a number of ends, tows, or strands collected into a parallel bundle with little or no twist.
2014-08-06
WIP Standard
AMS3904/12B
This specification covers one type of organic (para-aramid) fiber in the form of roving. The product shall be formed as a number of ends, tows, or strands collected into a parallel bundle with little or no twist.
2014-08-06
WIP Standard
AMS3904/1C
This specification covers one type of organic (para-aramid) fiber in the form of yarn. The product shall be formed as a multiplicity of filaments drawn together and gathered into an approximately parallel arrangement.
2014-08-06
WIP Standard
AMS3904/10B
This specification covers one type of organic (para-aramid) fiber in the form of roving. The product shall be formed as a number of ends, tows, or strands collected into a parallel bundle with little or no twist.
2014-08-06
WIP Standard
AMS3901D
This specification and its supplementary detail specifications cover organic fibers in the form of continuous, multifilament yarn and roving. These products have been used typically for use in weaving or as reinforcement in composites for structural applications, but usage is not limited to such applications. Each application should be considered individually.
2014-08-06
WIP Standard
AMS3901/8D
This specification covers one type of organic fiber in the form of yarn. The product shall be formed as a multiplicity of filaments drawn together and gathered into an approximately parallel arrangement. Organic 195 denier (215 d tex) yarn with 390 ksi (2689 MPa) or 21.0 g/d minimum tensile strength and 18 Msi (124 GPa) or 895 g/d minimum tensile modulus for use in weaving requiring high tensile strength and high modulus of elasticity in tension.
2014-08-06
WIP Standard
AMS3901/9D
This specification covers one type of organic fiber in the form of yarn. The product shall be formed as a multiplicity of filaments drawn together and gathered into an approximately parallel arrangement. Organic 380 denier (420 d tex) yarn with 390 ksi (2689 MPa) or 22.0 g/d minimum tensile strength and 17.5 Msi (121 GPa) or 850 g/d minimum tensile modulus for use in weaving requiring high tensile strength and high modulus of elasticity in tension.
2014-08-06
WIP Standard
AMS3901/14C
This specification covers one type of organic fiber in the form of yarn. The product shall be formed as a multiplicity of filaments drawn together and gathered into an approximately parallel arrangement.
2014-07-22
Standard
AMSC7438A
This specification covers treated aluminum core material for structural sandwich construction.
2014-03-20
WIP Standard
P1713AJ
To define the requirements for temperature (plus pressure and vacuum) measurement, control and calibration for composite processing equipment such as autoclaves, ovens and presses (perhaps) based on AMS2750E.
2013-12-11
WIP Standard
AMSSTD401A
This standard covers the general requirements and methods for testing sandwich core materials and for testing sandwich construction of the types used primarily in aircraft structures. This standard does not include test methods applicable only to a specific product; such test methods are included in the detailed specifications for the product.
2013-11-27
WIP Standard
P1713AI
This specification establishes the requirements for a #2511 epoxy resin preimpregnated T700SC-12K-50C Carbon Fiber Plain Weave Fabric product. The prepreg has a nominal fiber weight of 190 g/m2 (without sizing), and nominal resin content of 42% by weight.
2013-09-18
WIP Standard
P1713AF
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 250 °F. The composite may be used for the manufacture of primary and secondary aircraft structure. This is the basic spec and it will have three slash/detail specs.
2013-09-18
WIP Standard
P1713AE
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 250 °F. The composite may be used for the manufacture of primary and secondary aircraft structure. This is the first slash/detail spec.
2013-09-18
WIP Standard
P1713AH
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 250 °F. The composite may be used for the manufacture of primary and secondary aircraft structure. This is the third detail spec.
2013-09-18
WIP Standard
P1713AG
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 250 °F. The composite may be used for the manufacture of primary and secondary aircraft structure. This is the second detail spec.
2013-04-15
WIP Standard
AMS3960A
This specification establishes the requirements for a nominal 250 °F cure epoxy preimpregnated carbon fiber unidirectional tape product. This material is intended for use in laminate applications with a service temperature of -65 to 180 °F. The composite may be used for the manufacture of primary and secondary aircraft structure.
2013-04-15
WIP Standard
AMS3914A
This specification establishes the requirements for a nominal 250 °F cure epoxy preimpregnated carbon fiber plain weave fabric product. The prepreg is a plain weave fabric with 12K tows, a nominal fiber areal weight of 193 gsm, and nominal resin content of 42%. The purpose of this specification is to allow procurement of the material corresponding to the statistically derived material properties published in MIL-HDBK-17.
2013-04-15
WIP Standard
AMS3915A
This specification establishes the requirements for a nominal 250 °F cure epoxy preimpregnated 7781 glass fabric. The prepreg has a nominal fiber areal weight of 294 gsm, and nominal resin content of 38%.
2013-04-02
WIP Standard
P1713AB
Convert NCAMP NMS 128 Base Specification to AMS Format.
2013-04-02
WIP Standard
P1713AA
Convert NCAMP NMS 128/3 to AMS format
2013-04-02
WIP Standard
P1713AC
Convert NCAMP NMS 128/2 to AMS format
Viewing 1 to 30 of 272