49.025 : Materials for aerospace construction

49.025.01

Materials for aerospace construction in general

49.025.05

Ferrous alloys in general

49.025.10

Steels

49.025.15

Non-ferrous alloys in general

49.025.20

Aluminium

49.025.30

Titanium

49.025.40

Rubber and plastics

49.025.50

Adhesives

49.025.60

Textiles

49.025.99

Other materials
DIN EN 3479:2000-10

DIN EN 3479:2000-10

Superseded Historical

Aerospace series - Steel FE-PM1802 (X5CrNiCu15-5) consumable electrode remelted, solution treated and precipitation treated - Plate 6 mm < a 20 mm, 1070 MPa R 1220 MPa

€77.20

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ASTM D3039/D3039M-14

ASTM D3039/D3039M-14

Superseded Historical

Standard Test Method for Tensile Properties of Polymer Matrix Composite Materials

This product is not for sale, please contact us for more information

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NBN EN 4570:2020

NBN EN 4570:2020

Active Most Recent

Aerospace series - Heat resisting alloy X12CrNiCoMoW21-20 - Solution treated - Forgings - De = 100 mm

€58.00

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NBN EN 3510:2019

NBN EN 3510:2019

Active Most Recent

Aerospace series - Heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15) - Solution treated and precipitation treated - Bars and sections - De = 100 mm

€58.00

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NBN EN 4245:2020

NBN EN 4245:2020

Active Most Recent

Aerospace series - Heat resisting alloy FE-PM1708 - Vacuum arc remelted - As forged - Forging stock - De = 300 mm

€58.00

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NBN EN 4244:2020

NBN EN 4244:2020

Active Most Recent

Aerospace series - Heat resisting alloy FE-PM1708 - Vacuum arc remelted - Hardened and tempered - Bars - a or D = 200 mm - 1 000 MPa = Rm = 1 140 MPa

€58.00

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NBN EN 6064:2018

NBN EN 6064:2018

Active Most Recent

Aerospace series - Analysis of non-metallic materials (cured) for the determination of the extent of cure by Differential Scanning Calorimetry (DSC)

€58.00

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SAE AMS-P-46112A:2021-08-03

SAE AMS-P-46112A:2021-08-03

Active Most Recent

Plastic Sheet and Strip, Polyimide (Stabilized: Apr 2015)

€77.00

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SAE AMS 4416A:2012-10-03

SAE AMS 4416A:2012-10-03

Superseded Historical

Aluminum Alloy, Extruded Profiles (2196-T8511) 2.9Cu - 1.7Li - 0.4Mg - 0.4Ag - 0.10Zr Solution Heat Treated, Stress Relieved by Stretching and Artificially Aged

€68.00

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SAE AMS 5629E:2002-01-24

SAE AMS 5629E:2002-01-24

Superseded Historical

Steel, Corrosion Resistant, Bars, Forgings, Rings, and Extrusions, 13Cr 8.0Ni 2.2Mo 1.1Al Vacuum Induction Plus Consumable Electrode Melted Solution Heat Treated, Precipitation Hardenable

€94.00

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SAE AMS 5862J:2011-06-06

SAE AMS 5862J:2011-06-06

Superseded Historical

Steel, Corrosion-Resistant, Sheet, Strip, and Plate 15Cr - 4.5Ni - 0.30Cb (Nb) - 3.5Cu Consumable Electrode Remelted, Solution Heat Treated Precipitation-Hardenable

€81.00

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SAE AMS 6512G:2012-07-09

SAE AMS 6512G:2012-07-09

Superseded Historical

Steel, Maraging, Bars, Forgings, Tubing, and Rings 18Ni - 7.8Co - 4.9Mo - 0.40Ti - 0.10Al Consumable Electrode Vacuum Melted, Annealed

€81.00

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SAE AMS-QQ-A-250/11:1997-08-01

SAE AMS-QQ-A-250/11:1997-08-01

Superseded Historical

Aluminum Alloy 6061, Plate and Sheet

€77.00

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DIN EN 4632-004:2013-11

DIN EN 4632-004:2013-11

Active Most Recent

Aerospace series - Weldability and brazeability of materials in aerospace constructions - Part 004: Welding and brazing of homogeneous assemblies of high alloyed steels; German version EN 4632-004:2012

€105.42

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DIN EN 4632-006:2013-11

DIN EN 4632-006:2013-11

Active Most Recent

Aerospace series - Weldability and brazeability of materials in aerospace constructions - Part 006: Homogeneous assemblies of titanium alloys; German version EN 4632-006:2013

€91.03

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