EN 2155-12:1997
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Aerospace series - Test methods for transparent materials for aircraft glazing - Part 12: Determination of linear thermal expansion
Published date
07-23-1997
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This standard specifies the method to determine the reversible linear thermal expansion of plastics with exclusion of changes in length due to accidental factors such as changes in moisture content, degree of polymerization and stressrelease. Since it will not be possible to exclude all these accidental factors, the method can be expected to give only approximate values.
| Committee |
ASD-STAN
|
| DevelopmentNote |
Supersedes PREN 2155-12. (11/2003)
|
| DocumentType |
Standard
|
| PublisherName |
Comite Europeen de Normalisation
|
| Status |
Current
|
| Supersedes |
| Standards | Relationship |
| SNV DIN EN 2155-12 : 1997 | Identical |
| NEN EN 2155-12 : 1997 | Identical |
| NS EN 2155-12 : 1ED 1997 | Identical |
| UNI EN 2155-12 : 1998 | Identical |
| BS EN 2155-12:1997 | Identical |
| I.S. EN 2155-12:1998 | Identical |
| UNE-EN 2155-12:1998 | Identical |
| DIN EN 2155-12:1997-09 | Identical |
| PN EN 2155-12 : 2001 | Identical |
| NF EN 2155-12 : 1997 | Identical |
| NBN EN 2155-12 : 1997 | Identical |
| DIN V EN 2155-12:1986-12 | Identical |
| PREN 2314 : 1 | AEROSPACE SERIES - SHOCK RESISTANT ACRYLIC SHEETS FOR AIRCRAFT GLAZING - TECHNICAL SPECIFICATION |
| PREN 4366 : 200P1 | AEROSPACE SERIES - HEAT AND CRAZING RESISTANT CAST ACRYLIC, CROSSLINKED, MULTI-AXIALLY STRETCHED, AND LOW MOISTURE ABSORPTION - PROPERTIES |
| PREN 2343 : 2 | AEROSPACE SERIES - HEAT AND CRAZING RESISTANT CAST AND MULTI-AXIALLY ORIENTATED ACRYLIC SHEETS FOR AIRCRAFT GLAZING - TECHNICAL SPECIFICATION |
| PREN 2719 : 200P1 | AEROSPACE SERIES - POLYCARBONATE SHEET - TECHNICAL SPECIFICATION |
| PREN 4243 : 200P1 | AEROSPACE SERIES - CAST ACRYLIC SHEETS - TECHNICAL SPECIFICATION |
| PREN 4364 : 200P1 | AEROSPACE SERIES - CAST ACRYLIC - PROPERTIES |
| PREN 2155 : 1 | AEROSPACE SERIES - TEST METHODS FOR TRANSPARENT MATERIALS FOR AIRCRAFT GLAZING |
| PREN 2833-3 : 200P1 | AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 3: GLASS FABRIC/EPOXY RESIN PREIMPREGNATE CURING AT UP 180 DEGREES C FOR CONTINUOUS USE UP TO 120 DEGREES C |
| PREN 2833-2 : 200P1 | AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 2: GLASS FABRIC/EPOXY RESIN PREIMPREGNATES CURING AT UP 125 DEGREES C FOR CONTINUOUS USE UP TO 80 DEGREES C |
| 97/713394 DC : DRAFT AUG 1997 | PREN 4365 - AEROSPACE STANDARD - HEAT AND CRAZING RESISTANT ACRYLIC - CAST AND CROSS LINKED - LOW MOISTURE ABSORPTION - PROPERTIES |
| 97/713392 DC : DRAFT AUG 1997 | PREN 4243 - AEROSPACE SERIES - ACRYLIC (PMMA) SHEETS - TECHNICAL SPECIFICATION |
| PREN 2342 : 1 | AEROSPACE SERIES - HEAT AND CRAZING RESISTANT ACRYLIC SHEETS FOR AIRCRAFT GLAZING - TECHNICAL SPECIFICATION |
| PREN 4365 : 200P1 | AEROSPACE SERIES - HEAT AND CRAZING RESISTANT CAST ACRYLIC, CROSSLINKED, AND LOW MOISTURE ABSORPTION - PROPERTIES |
| 97/713393 DC : DRAFT AUG 1997 | PREN 4364 - AEROSPACE STANDARD - CAST (PMMA) ACRYLIC - PROPERTIES |
| 97/713388 DC : DRAFT AUG 1997 | PREN 2719 - AEROSPACE SERIES - POLYCARBONATE SHEET - TECHNICAL SPECIFICATION |
| UNI EN 2833-005 : 2014 | AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 005: GLASS FABRIC/PHENOLIC RESIN PREIMPREGNATE |
| PREN 2833-5 : 200P1 | AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 5: GLASS FABRIC/PHENOLIC RESIN PREIMPREGNATE |
| I.S. EN 2833-005:2013 | AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 005: GLASS FABRIC/PHENOLIC RESIN PREIMPREGNATE |
| 97/713395 DC : DRAFT AUG 1997 | PREN 4366 - AEROSPACE STANDARD - HEAT AND CRAZING RESISTANT ACRYLIC - CAST, CROSSLINKED AND MULTI-AXIALLY STRETCHED - LOW MOISTURE ABSORPTION - PROPERTIES |
| XP PREN 2833-2 : 1995 XP | AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 2: GLASS FABRIC/EPOXY RESIN PREIMPREGNATES CURING AT UPTO 125 DEGREES C FOR CONTINUOUS USE UPTO 80 DEGREES C |
| EN 2833-005:2013 | Aerospace series - Glass fibre thermosetting preimpregnates - Technical specification - Part 005: Glass fabric/phenolic resin preimpregnate |
| 95/714421 DC : 0 | PREN 2833-3 - AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 3: GLASS FABRIC/EPOXY RESIN PREIMPREGNATE CURING AT UP TO 180 DEGREE C FOR CONTINUOUS USE UP TO 120 DEGREE C |
| 93/711194 DC : 0 | PREN 2833-2 - TECHNICAL SPECIFICATION - GLASS FIBRE THERMOSETTING PREIMPREGNATES - PART 2: GLASS FABRIC/EPOXY RESIN PREIMPREGNATES CURING AT 125 DEGREES C FOR CONTINUOUS USE UP TO 80 DEGREES C |
| BS EN 2833-005:2013 | Aerospace series. Glass fibre thermosetting preimpregnates. Technical specification Glass fabric/phenolic resin preimpregnate |
| 95/714422 DC : 0 | PREN 2833-4 - AEROSPACE SERIES - GLASS FIBER THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 4: UNIDIRECTIONAL GLASS/EPOXY RESIN PREIMPREGNATE CURING AT UP TO 125 DEGREE C FOR CONTINUOUS USE UP TO 80 DEGREE C |
| PREN 2263 : 2 | AEROSPACE SERIES - POLYMETHYL METHACRYLATE (AS CAST) SHEETS FOR AIRCRAFT GLAZING - TECHNICAL SPECIFICATION |
| PREN 2833-4 : 200P1 | AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 4: UNIDIRECTIONAL GLASS/EPOXY RESIN PREIMPREGNATE CURING AT UP TO 125 DEGREES C FOR CONTINUOUS USE UP TO 80 DEGREES C |
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