Composites Technology - FSC CMPS

MIL-F-64156 - Fabric, Carbon (Graphite) Fiber, Nickel-Coated

This specification establishes the requirements for nickel-coated carbon (graphite) yarn and woven fiber cloth for use as a conductive surface ply to provide lighting strike protection to composites structures. Materials described herein are typically impregnated with a compatible epoxy resin.

MIL-F-87121 - Fabric, Graphite Fiber

This specification covers the materials requirements and quality assurance provisions for an eight harness satin weave graphite fabric.

MIL-G-47024 - Glass Roving, Phenolic Impregnated

MIL-HDBK-17/2 - Composite Materials Handbook Volume 2. Polymer Matrix Composites Materials Properties (S/S By Sae-R423))

A primary focus of this Handbook is guidance on the selection and use of composite materials. The data collected within this volume are presented to allow initial assessments of material adequacy for a particular application. It provides a common database that will allow significant reductions in the amount of validation data necessary to use the data for design purposes. This handbook cannot be cited as a DoD contractor requirement.

MIL-HDBK-17/3 - Composite Materials Handbook Volume 3. Polymer Matrix Composites Materials Usage, Design, And Analysis (S/S By Sae-R424))

Volume 3 of MIL-HDBK-17 provides methodologies and lessons learned for the design, analysis, manufacture, and field support of fiber-reinforced, polymeric-matrix composite structures. It also provides guidance on material and process specifications and procedures for utilization of the material data presented in Volume 2. The information provided is consistent with the guidance provided in Volume 1 and intended to be an extensive compilation of the current "best knowledge and practices" of composite materials and structures engineers and scientists from industry, government, and academia. This volume will be continually updated as the "state-of-the-art" of composites technology advances.

MIL-HDBK-17 - Polymer Matrix Composites, Volume 1. Guidelines (S/S By Mil-Hdbk-17/1)

Volume I - Provides guidelines for the characterization of composite material systems to be used in aerospace vehicles and structures. Composite material systems must normally be evaluated in accordance with these, or equivalent guidelines, in order to be considered acceptable by government certification and procuring agencies. Volume II - Will provide a compilation of statistically-based mechanical property data for current and emerging composite material systems used in the aerospace industry. B-basis strength and strain-to-failure values will be presented along with related data. Volume III - Will provide information regarding materials and fabrication procedures, quality control, and design and analysis.

MIL-HDBK-401 - Hot Isostatic Processing

The purpose of this handbook is to provide selective information on the hot isostatic process to establish its potential application to parts and components for usage in military vehicles.

MIL-M-46196 - Metal Matrix Composites (Mmc): Aluminum Reinforced With Silicon Carbide Particles Or Whiskers

This specification establishes the requirements and tests for aluminum reinforced with silicon carbide particles or whiskers metal matrix composite (MMC) products.

MIL-M-64157 - Metal Matrix Composites (Mmc): Carbon (Graphite) Fiber Reinforced/Aluminum, General Specification For

This general specification and asociated detail specifications define the material property, processing and test method requirements for carbon (graphite) fiber reinforced aluminum (Gr/AI) metal matrix composites (MMC) intended for military aerospace applications.

MIL-M-64157/1 - Metal Matrix Composites (Gr/Al): Standard Electronic Module (Sem) Format E Heatsink

This detail specification in association with the general specification covers the requirements for a graphite/aluminum metal matrix composite module frame of the Standard Electronic Module Format E (SEM E).

MIL-M-64157/2 - Metal Matrix Composites (Gr/Al): Space Radiator Panels

This detail specification in association with the general specification covers the requirements for carbon (graphite)/aluminum metal matrix composites for spacecraft radiators used for thermal management.

MIL-M-64157/3 - Metal Matrix Composites (Gr/Al): Tubes For Truss Structures

This detail specification covers the requirements for carbon (graphite)/aluminum metal matrix composite tubes intended for space truss structures.

MIL-M-64158 - Metal Matrix Composites (Mmc): Continuous Silicon Carbide Fiber Reinforced/6061 Aluminum

This specification establishes the requirements for 6061 aluminum matrix MMC's reinforced with silicon carbide fiber making up at least 45 volume percent of the material.

MIL-P-87123 - Preform, Rigidized, Graphite Fiber, 3D, Fineweave Pierced Fabric

This specification establishes the requirements and quality assurance provisions for rigidized graphite fiber reinforced 3D, fineweave pierced fabric preforms.

MIL-P-87124 - Pitch, Coal Tar

This specification establishes the requirements and quality assurance provisions for, vacuum coal-tar pitch for the densification of carbon- carbon composites.

MIL-P-9400 - Plastic Laminate And Sandwich Construction Parts And Assembly, Aircraft Structural, Process Specification Requirements

This specification provides detailed instructions for the preparation of, and requirements to be included in, process specifications required for the processing, inspection, pre-fit, and assembly of structural plastic laminate and sandwich construction parts for aircraft.

MIL-PRF-46103 - Armor: Lightweight, Composite

This specification covers the performance requirements for lightweight composite armor (see 6.1).

MIL-PRF-46187 - Prepreg, Unidirectional Tape, Carbon (Graphite) Fiber High Temperature Resin Impregnated, 316 Deg. C (600 Deg. F)

This specification establishes the requirements for carbon fiber/high temperature resin prepreg in the form of unidirectional tape suitable for the fabrication of structural laminates intended for use at temperatures up to and including 316 Deg. C (600 Deg. F) (see 6.1).

MIL-PRF-46190 - Prepregs, Woven Fabric, Carbon Fiber, Resin Impregnated

This specification establishes the requirements for resin impregnated, high strength, carbon fiber, woven fabric prepregs (see 6.11.

MIL-PRF-46197 - Laminate: High-Strength Glass, Fabric-Reinforced, Polyester Resin Preimpregnated

This specification establishes the requirements for a high strength woven glass roving impregnated with polyester resin for molding thick armored vehicle structures.

MIL-PRF-47257 - Compound, Epoxy, Filament Winding

This specification covers a fiberglass roving impregnated with an epoxy resin-hardener compound used in the fabrication of filament wound structures.

MIL-R-87120 - Rods, Pultruded, Graphite Fiber Reinforced, Processing Of

This specification establishes the processing requirements and quality assurance provisions for pultruded rods.

MIL-STD-2031 - Fire And Toxicity Test Methods And Qualification Procedure For Composite Material Systems Used In Hull, Machinery, And Structural Applications Inside Naval Submarines

MIL-STD-368 - Hplc Of Pmr-15 Polyimide Resin And Prepregs (S/S By Mil-Hdbk-368)

This standard prescribes test methods for the high performance liquid chromatography (HPLC) of PMR-15 polyimide resin and prepreg materials.

MIL-STD-373 - Transverse Tensile Properties Of Undirectional Fiber/Resin Composite Cylinders (S/S By Astm-D5450/D5450M)

This test method covers the determination of the transverse tensile properties of hoop wound resin matrix composites reinforced by high-modulus (greater than 21 GPa or 3 Msi), continuous fibers.

MIL-STD-374 - Transverse Compressive Properties Of Unidirectional Fiber/Resin Composite Cylinders (S/S By Astm-D5449/D5449M)

This test method covers the determination of the transverse compressive properties of hoop wound resin matrix composites reinforced by high modulus (greater than 21 GPa or 3 Msi), continuous fibers.

MIL-STD-375 - In-Plane Shear Properties Of Unidirectional Fiber/Resin Composite Cylinders (S/S By Astm-D5448/D5448M)

This test method covers the determination of the in-plane shear properties of hoop wound resin matrix composites reinforced by high-modules (greater than 21 GPa or 3 Msi), continuous fibers.

MIL-T-29586 - Thermosetting Polymer Matrix, Unidirectional Carbon Fiber Reinforced Prepreg Tape (Widths Up To 60 Inches), General Specification For

This specification establishes the general requirements for termosetting polymer matrix, unidirectional carbon fiber prepregs. Specific requirements for the prepreg material are governed by this document along with the applicable specification sheet. This specification contains qualification requirements. Qaulification pertains only to the requirements of this specification and does not qualify the material for use in the fabrication of a structural component in a particular system. Qualifying a material for use in the fabrication of a structural component requires additional testing requirements as determined by the government and the system manufacturer (see 6.3).

MIL-T-29586/1 - Thermosetting Polymer (Epoxy) Matrix, 350 Deg. F(177 Deg. C) Cure, Intermediate Modulus Carbon Fiber Reinforced Prepreg Tape, (Widths Up To 60 Inches)

MIL-Y-83370 - Yarn, Roving, And Cloth: High Modulus, Organic Fiber

MIL-Y-83371 - Yarns, Graphite, High Modulus, Continuous Filament

MIL-Y-87125 - Yarn, Graphite, 1000/3000 Filaments

This specification establishes the requirements and quality assurance provisions for continuous filament high modulus graphite yarn derived from pyrolyzed polyacrylonitrile filaments.

SACMA-SRM1 - Compressive Properties Of Oriented Fiber-Resin Composites, Recommended Test Method For

This method covers the procedure for the determination of the compressive properties of fiber-resin composites reinforced by oriented continuous high modulus , >3x10 6psi, fibers

SACMA-SRM10 - Composite Test Laminates, Calculation Of Fiber Volume Of, Recommended Method For

This standard method covers the determination of the Fiber Volume content. It will be depicted as a percentage of reinforcing fiber volume versus the total laminate volume.

SACMA-SRM12 - Lot Acceptance Of Carbon Fibers, Recommended Method For

This method describes lot acceptance procedures for carbon and grphite fibers in the form of continuous multifilament tows and yarns.

SACMA-SRM13 - Determination Of Mass Per Unit Length Of Carbon Fibers, Recommended Test Method For

This method covers the procedure for the determination of Mass Per Unit Length (MUL) of carbon fiber.

SACMA-SRM14 - Determination Of Sizing Content On Carbon Fibers, Recommended Test Method For

SACMA-SRM15 - Determination Of Density Of Carbon Fibers, Recommended Test Method For

This method covers the procedure for the determination of density of carbon fiber by the Archimedes Principle.

SACMA-SRM16 - Tow Tensile Testing Of Carbon Fibers, Recommended Test Method For

This method covers the procedure for the determination of tensile properties (strength and modulus) of carbon fibers.

SACMA-SRM17 - Determination Of Twist In Carbon Fibers, Recommended Test Method For

SACMA-SRM2 - Compression After Impact Properties Of Oriented Fiber-Resin Composites, Recommended Test Method For

This method covers the procedure for the determination of the compression after impact properties of fiber-resin composites reinforced by oriented continuous high modulus, > 3x10 6 psi, fibers.

SACMA-SRM3 - Open-Hole Compression Properties Of Oriented Fiber-Resin Composites, Recommended Test Method For

This method covers the procedure for the determination of the compression properties of fiber-resin composite laminated reinforced by continuous, high modulus,>3x10 6 psi, fibers containing a circular hole.

SACMA-SRM4 - Tensile Properties Of Oriented Fiber-Resin Composites, Recommended Test Method Of

This test method covers the procedure for the determination of the tensile properties of oriented fiber-resin composites reinforced by oreinted contiuous high modulus. >3x10 6 psi, fibers.

SACMA-SRM5 - Open-Hole Tensile Properties Of Oriented Fiber-Resin Composites, Recommended Test Method Of

This test method covers the procedure for the determination of the tensile properties of oriented fiber-resin composite laminates reinforced by oriented continuous high modulus, >3x10 6psi, fibers containing a circular hole.

SACMA-SRP1 - Printing And Applying Bar Code Labels, Recommended Practice For

This recommended practice provides guidelines for pinting and applying bar code labels for identification and shipment of composite prepregs, carbon and aramid fibers, as well as other products sold by composite materials suppliers.