MIL-HDBK-349 Base Document:1994
|
MANUFACTURE AND INSPECTION OF ADHESIVE BONDED, ALUMINUM HONEYCOMB SANDWICH ASSEMBLIES FOR AIRCRAFT |
17/30342710 DC : 0
|
BS EN ISO 12215-5 - SMALL CRAFT - HULL CONSTRUCTION AND SCANTLINGS - PART 5: DESIGN PRESSURES FOR MONOHULLS, DESIGN STRESSES, SCANTLINGS DETERMINATION |
ASTM D 6416/D6416M : 2016 : REDLINE
|
Standard Test Method for Two-Dimensional Flexural Properties of Simply Supported Sandwich Composite Plates Subjected to a Distributed Load |
ASTM C 481 : 1999
|
Standard Test Method for Laboratory Aging of Sandwich Constructions |
93/706616 DC : 0
|
PREN 2833-1 - AEROSPACE SERIES - TECHNICAL SPECIFICATION - GLASS FIBER THERMOSETTING PREIMPREGNATES - PART 1: GENERAL |
ASTM C 481 : 1999 : R2005
|
Standard Test Method for Laboratory Aging of Sandwich Constructions |
ASTM C 480 : 1999 : R2005
|
Standard Test Method for Flexure Creep of Sandwich Constructions |
ISO 12215-5:2008
|
Small craft Hull construction and scantlings Part 5: Design pressures for monohulls, design stresses, scantlings determination |
SAE AS 8056 : 2004(R2016)
|
MINIMUM DESIGN AND PERFORMANCE OF AIRPLANE GALLEY IN-FLIGHT CARTS, CONTAINERS, AND ASSOCIATED COMPONENTS |
ASTM C 481 : 1999 : R2011
|
Standard Test Method for Laboratory Aging of Sandwich Constructions |
ASTM C 480 : 1999
|
Standard Test Method for Flexure Creep of Sandwich Constructions |
DIN EN ISO 12215-5:2014-10
|
SMALL CRAFT - HULL CONSTRUCTION AND SCANTLINGS - PART 5: DESIGN PRESSURES FOR MONOHULLS, DESIGN STRESSES, SCANTLINGS DETERMINATION (ISO 12215-5:2008 + AMD 1:2014) |
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] |
UNI EN ISO 12215-5 : 2014
|
SMALL CRAFT - HULL CONSTRUCTION AND SCANTLINGS - PART 5: DESIGN PRESSURES FOR MONOHULLS, DESIGN STRESSES, SCANTLINGS DETERMINATION |
PREN 2833-1 : 200P2
|
AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 1: GENERAL REQUIREMENTS |
SAE AMS 3710 : 2014
|
SANDWICH STRUCTURES, GLASS FABRIC-RESIN, LOW PRESSURE MOLDED, HEAT RESISTANT |
SAE AMS STD 401 : 1999
|
SANDWICH CONSTRUCTIONS AND CORE MATERIALS - GENERAL TEST METHODS |
BS EN ISO 12215-5 : 2008
|
SMALL CRAFT - HULL CONSTRUCTION AND SCANTLINGS - PART 5: DESIGN PRESSURES FOR MONOHULLS, DESIGN STRESSES, SCANTLINGS DETERMINATION |
UNE-EN ISO 12215-5:2008
|
Small craft - Hull construction and scantlings - Part 5: Design pressures for monohulls, design stresses, scantlings determination (ISO 12215-5:2008) |
SAE AMS 3970/1 : 2011
|
CARBON FIBER FABRIC REPAIR PREPREG, 120 DEGREES C (250 DEGREES F) VACUUM CURING - PART 1 - GENERAL REQUIREMENTS |
NF EN ISO 12215-5 : 2008 AMD 1 2014
|
SMALL CRAFT - HULL CONSTRUCTION AND SCANTLINGS - PART 5: DESIGN PRESSURES FOR MONOHULLS, DESIGN STRESSES, SCANTLINGS DETERMINATION |
MIL-STD-401 Revision B:1967
|
SANDWICH CONSTRUCTIONS AND CORE MATERIALS, GENERAL TEST METHODS |
ASTM C 481 : 1999 : R2016
|
Standard Test Method for Laboratory Aging of Sandwich Constructions |
I.S. EN ISO 12215-5:2008
|
SMALL CRAFT - HULL CONSTRUCTION AND SCANTLINGS - PART 5: DESIGN PRESSURES FOR MONOHULLS, DESIGN STRESSES, SCANTLINGS DETERMINATION (ISO 12215-5:2008) |
EN ISO 12215-5:2008/A1:2014
|
SMALL CRAFT - HULL CONSTRUCTION AND SCANTLINGS - PART 5: DESIGN PRESSURES FOR MONOHULLS, DESIGN STRESSES, SCANTLINGS DETERMINATION (ISO 12215-5:2008/AMD 1:2014) |
SAE AMS A 25463 : 2013
|
ADHESIVE, FILM FORM, METALLIC STRUCTURAL SANDWICH CONSTRUCTION |
SAE AMS 3715 : 2013
|
CORE, HONEYCOMB, GLASS/PHENOLIC |
MIL-A-25463 Revision B:1982
|
ADHESIVE, FILM FORM, METALLIC STRUCTURAL SANDWICH CONSTRUCTION |
15/30274132 DC : 0
|
BS ISO 18402 - TESTING STRUCTURES - STRUCTURAL INSULATED PANEL ROOF CONSTRUCTION - TEST METHODS |