ASTM C 393 : 2000
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
Standard Test Method for Flexural Properties of Sandwich Constructions
Hardcopy , PDF
11-11-2014
English
10-01-2000
Important note : Users cannot be edited or removed once added to your Multi user PDF.CONTAINED IN VOL. 15.03, 2005 Determines the properties of flat sandwich constructions exposed to flat wise flexure in such a way that the applied moments create curvature of the sandwich facing planes.
| Committee |
D 30
|
| DocumentType |
Test Method
|
| Pages |
4
|
| PublisherName |
American Society for Testing and Materials
|
| Status |
Superseded
|
| SupersededBy |
1.1 This test method covers determination of the properties of flat sandwich constructions subjected to flatwise flexure in such a manner that the applied moments produce curvature of the sandwich facing planes.
1.2 The values stated in SI units are to be regarded as the standard. The inch-pound units given may be approximate.
1.3 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use.
| 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) |
| 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 |
Access your standards online with a subscription
Features
-
Simple online access to standards, technical information and regulations.
-
Critical updates of standards and customisable alerts and notifications.
-
Multi-user online standards collection: secure, flexible and cost effective.