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DIN - WL 8.3621 - AEROSPACE SERIES - CARBON FIBRES, HIGH PERFORMANCE CARBON FIBRE FILAMENT YARNS - FIBRE MATERIAL CLASS G, 200 TEX, F 3000; INACTIVE FOR NEW DESIGN Organization: DIN
Date: 2003-06-01
DIN - WL 8.3632 - AEROSPACE SERIES - CARBON FIBRES, HIGH PERFORMANCE CARBON FIBRE FILAMENT YARNS - FIBRE MATERIAL CLASS H, 400 TEX, F 6000; INACTIVE FOR NEW DESIGN Organization: DIN
Date: 2003-06-01
DNVGL-CP-0096 - CARBON FIBRE TOWS Organization: DNVGL
Date: 2016-03-01
Description: This CP gives a description of the procedures and requirements related to documentation, design and type testing applicable for TA of carbon fibre tows. TA is based on compliance with material requirements given in the Society's rules and/or other regulations and standards.
DESTECH - FUNDAMENTALS OF FIBER SCI - FUNDAMENTALS OF FIBER SCIENCE Organization: DESTECH
Date: 2014-01-01
Description: Technologies in this text apply to the analysis and design of fibers for industrial, electronic, optical, medical and energy storage applications.
GMW15703 - TWO-COMPONENT URETHANE CLEARCOAT OVER EXTERIOR EXPOSED CARBON FIBER - ISSUE 2; ENGLISH Organization: GMW
Date: 2013-01-01
Description: These clearcoats are designed to be applied directly to GM approved carbon fiber substrates. Parts coated in this manner are typically used on the exterior of the vehicle and are designed to meet exterior durability performance requirements.
SAE T-124 - AUTOMOTIVE CARBON FIBER COMPOSITES FROM EVOLUTION TO IMPLEMENTATION - TO PURCHASE CALL 1-800-854-7179 USA/CANADA OR 303-397-7956 WORLDWIDE Organization: SAE
Date: 2011-11-29
Description: Executive Summary The advantages of carbon fiber composites (CFCs) in automotive design are high stiffness, high specific strength (strength-to-weight ratio), excellent fatigue endurance, corrosion resistance, generally good impact resistance, and flexibility in design that permits them to be tailored to design requirements.
TIA-598 - OPTICAL FIBER CABLE COLOR CODING Organization: TIA
Date: 2014-07-09
Description: Conversely, most cables deployed outdoors must incorporate additives in the jacket material to be able to withstand the damaging effects of solar radiation over their designed operating lifetime. Such products typically contain carbon black material to provide the requisite level of protection, which precludes the use of any jacket color other than black.
ASTM C1783 - STANDARD GUIDE FOR DEVELOPMENT OF SPECIFICATIONS FOR FIBER REINFORCED CARBON-CARBON COMPOSITE STRUCTURES FOR NUCLEAR APPLICATIONS Organization: ASTM
Date: 2015-09-01
Description: This document is a guide to preparing material specifications for fiber reinforced carbon-carbon (C-C) composite structures (flat plates, rectangular bars, round rods, and tubes) manufactured specifically for structural components in nuclear reactor core applications. The carbon-carbon composites consist of carbon/graphite fibers (from PAN, pitch, or rayon precursors) in a carbon/graphite matrix produced by liquid infiltration/pyrolysis and/or by chemical vapor infiltration.
GMW17667 - LIMITED DURABILITY TWO-COMPONENT URETHANE CLEARCOAT OVER EPOXY BASE EXTERIOR EXPOSED WEAVE CARBON FIBER - ISSUE 1; ENGLISH Organization: GMW
Date: 2016-10-01
Description: These clearcoats are designed to be applied directly to GM approved epoxy based exposed weave carbon fiber substrates.
NPFC - MIL-PRF-46187 - PREPREG, UNIDIRECTIONAL TAPE, CARBON (GRAPHITE) FIBER HIGH TEMPERATURE RESIN IMPREGNATED, 316 DEG. C (600 DEG. F) Organization: NPFC
Date: 1998-08-14
Description: 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°C (600°F) (see 6.1).
DNVGL-CP-0434 - UNI- AND MULTI-AXIAL MULTI-PLY FABRICS MADE OF CARBON FIBRES - INCORPORATES AMENDMENT: APRIL 2016 Organization: DNVGL
Date: 2015-12-01
Description: This CP gives a description of the procedures and requirements related to documentation, design and type testing applicable for TA of carbon fibre fabrics. TA is based on compliance with material requirements given in the rules and/or other regulations and standards.
NASA-LLIS-0689 - LESSONS LEARNED – FIBER-REINFORCED POLYMER COMPOSITE MATERIAL SELECTION Organization: NASA
Date: 2000-03-09
Description: This is especially true in the case of advanced composite materials with polymer matrices reinforced with carbon or aramid (Kevlar®) fibers. The important considerations necessary for a proper selection of a fiber-reinforced polymer composite material in NASA spacecraft and satellite structures include fiber material, fiber reinforcement form, fiber volume, matrix material, ply lamination, processing, cost, database, health and safety factors and end-item properties.
NAVY - 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) Organization: NAVY
Date: 1991-04-30
Description: This specification in conjunction with MIL-T-29586(AS) establishes the requirements for a 350°F(177°C) cured epoxy prepreg reinforced with intermediate modulus unidirectional carbon fiber tow. - As specified in the contract or purchase order, the prepreg tape material shall be supplied in the Classes specified in Table I.
BRE IP14/14 - NATURAL FIBRE REINFORCED POLYMERS (NFRPS) IN THE CONSTRUCTION INDUSTRY Organization: BRE
Date: 2014-11-01
Description: In FRP composites a polymer resin (also called ‘matrix') is reinforced with fibres. The most commonly used fibres are glass and carbon, the most commonly used resin is thermoset epoxy or polyester-based.
ISO 11119-1 - GAS CYLINDERS - REFILLABLE COMPOSITE GAS CYLINDERS AND TUBES - DESIGN, CONSTRUCTION AND TESTING - PART 1: HOOP WRAPPED FIBRE REINFORCED COMPOSITE GAS CYLINDERS AND TUBES UP TO 450 - SECOND EDITION Organization: ISO
Date: 2012-08-01
Description: This part of ISO 11119 is limited to cylinders and tubes with composite reinforcement of carbon fibre, aramid fibre or glass fibre (or a mixture thereof) within a matrix or steel wire to provide circumferential reinforcement.
ISO 11119-4 - GAS CYLINDERS - REFILLABLE COMPOSITE GAS CYLINDERS - DESIGN, CONSTRUCTION AND TESTING - PART 4: FULLY WRAPPED FIBRE REINFORCED COMPOSITE GAS CYLINDERS UP TO 150 L WITH LOAD-SHARING WELDED METALLIC LINERS - FIRST EDITION Organization: ISO
Date: 2016-02-15
Description: The cylinders are constructed in the form of a welded stainless steel liner or welded ferritic steel liner or welded aluminium alloy liner and overwrapped with carbon fibre or aramid fibre or glass fibre (or a mixture thereof) in a matrix to provide longitudinal and circumferential reinforcement.
ISO 11119-3 - GAS CYLINDERS - REFILLABLE COMPOSITE GAS CYLINDERS AND TUBES PART 3: FULLY WRAPPED FIBRE REINFORCED COMPOSITE GAS CYLINDERS AND TUBES UP TO 450L WITH NON-LOAD-SHARING METALLIC OR NON-METALLIC LINERS - SECOND EDITION Organization: ISO
Date: 2013-04-15
Description: The cylinders are constructed: 1) in the form of a disposable mandrel overwrapped with carbon fibre or aramid fibre or glass fibre (or a mixture thereof) in a resin matrix to provide longitudinal and circumferential reinforcement; 2) in the form of two filament wound shells joined together.
SAE/TP - 2009-01-3184 - NEW BLIND, DOWELING, TEMPORARY FASTENER DESIGN AND TESTING Organization: SAE/TP
Date: 2009-11-10
Description: This paper illustrates how these new fasteners work and how they are designed. Results of some testing of nominal ¼", flush head fasteners in carbon-fiber reinforced plastic are shown.
SAE PT-166 - CAE DESIGN AND FAILURE ANALYSIS OF AUTOMOTIVE COMPOSITES - TO PURCHASE CALL 1-800-854-7179 USA/CANADA OR 303-397-7956 WORLDWIDE Organization: SAE
Date: 2014-12-03
Description: The primary reason is that those properties are dependent upon the fiber volume fractions. Even for the same composite system, such as the carbon fiber–epoxy composite, the basic lamina properties vary dramatically due to the amount of fibers used in the system.
DS/EN 14427 - LPG EQUIPMENT AND ACCESSORIES - TRANSPORTABLE REFILLABLE FULLY WRAPPED COMPOSITE CYLINDERS FOR LPG - DESIGN AND CONSTRUCTION Organization: DS
Date: 2014-06-23
Description: This European Standard - specifies minimum requirements for materials, design, construction, prototype testing and routine manufacturing inspections of fully wrapped composite cylinders with a water capacity from 0,5 litre up to and including 150 litres for liquefied petroleum gases (LPG) exposed to ambient temperatures, with a test pressure of at least 30 bar; - is only applicable to cylinders which are fitted with a pressure relief valve (see 4.1.3); - is applicable to cylinders with a liner of metallic material (welded or seamless) or non-metallic material (or a mixture thereof), reinforced by fibres of glass, carbon or aramid (or a mixture thereof); - is also applicable to composite cylinders without liners.

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