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SAE AMS C 9084 : 2013

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by

CLOTH, GLASS, FINISHED, FOR RESIN LAMINATES

Available format(s)

Hardcopy , PDF

Superseded date

06-03-2024

Superseded by

SAE AMSC9084:1999(R2022)

Language(s)

English

Published date

17-07-2013

€116.29
Excluding VAT

NOTICE
1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PREPARATION FOR DELIVERY
6. NOTES

Describes woven glass cloth which has been suitably finished for further fabrication into glass fabric base resin laminates and sandwich materials.

Committee
AMS P17
DevelopmentNote
Supersedes MIL C 9084 (C). (07/2013)
DocumentType
Standard
Pages
17
PublisherName
SAE International
Status
Superseded
SupersededBy
Supersedes

Standards Relationship
MIL-C-9084 Revision C:1970 Similar to

MIL-STD-2199 Revision A:2010 COVERINGS FOR WATERBORNE MAIN PROPULSION SHAFTING ON U.S. NAVAL SURFACE SHIPS AND SUBMARINES
MIL-PRF-24667 Revision C:2008 COATING SYSTEM, NON-SKID, FOR ROLL, SPRAY, OR SELF-ADHERING APPLICATION
SAE ARP 5606 : 2011 COMPOSITE HONEYCOMB NDI REFERENCE STANDARDS
ASTM E 1556 : 2012 : REDLINE Standard Specification for Epoxy Resin System for Composite Skin, Honeycomb Sandwich Panel Repair
MIL-DTL-64154 Revision B:2008 LAMINATE: FIBERGLASS-FABRIC-REINFORCED, PHENOLIC
NFPA 1150 : 2017 FOAM CHEMICALS FOR FIRES IN CLASS A FUELS
MIL-DTL-25421 Revision C:2009 Plastic Materials, Glass Fiber Base - Epoxy Resin, Low Pressure Laminated
SAE AMS 3970/6 : 2011 CARBON FIBER FABRIC REPAIR PREPREG, 120 DEGREES C (250 DEGREES F) VACUUM CURING - PART 6 - MATERIAL SPECIFICATION: CARBON FIBER FABRIC REINFORCED EPOXY PREPREG FOR REPAIR, PLAIN WEAVE FABRIC, 193 G/M[2], ADHESIVE FILM FOR REPAIR AND NON-STRUCTURAL GLASS FIBER FABRIC REINFORCED EPOXY PREPREG, 105 G/M[2]
SAE AMS 3915 : 2015 ADVANCED COMPOSITES PREPREG - NOMINAL 250 DEGREES F CURE - GLASS FIBER AND EPOXY RESIN, 7781 WEAVE FABRIC
SAE AMS 3970/1 : 2011 CARBON FIBER FABRIC REPAIR PREPREG, 120 DEGREES C (250 DEGREES F) VACUUM CURING - PART 1 - GENERAL REQUIREMENTS

MIL-R-9299 Revision C:1968 RESIN, PHENOLIC, LAMINATING
MIL-R-25506 Revision C:1982 Resin Solution, Silicone, Low-Pressure Laminating
PPP-P-1133 Revision C:1983 PACKAGING OF SYNTHETIC FIBER FABRICS
FED-STD-406 Revision A:1982 PLASTIC, METHODS OF TESTING
MIL-R-7575 Revision C:1966 Resin, Polyester, Low-Pressure Laminating
MIL-Y-1140 Revision H:1972 Yarn, Cord, Sleeving, Cloth, and Tape-Glass
FED-STD-191 Revision A:1978 TEXTILE TEST METHODS
MIL-R-9300 Revision B:1968 RESIN, EPOXY, LOW-PRESSURE LAMINATING
MIL-STD-105 Revision E:1989 SAMPLING PROCEDURES AND TABLES FOR INSPECTION BY ATTRIBUTES

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