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
ASTM E1235-12(2025)

ASTM E1235-12(2025)

Active Most Recent

Standard Test Method for Gravimetric Determination of Nonvolatile Residue (NVR) in Environmentally Controlled Areas for Spacecraft

€72.00

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BS EN 3527:2025

BS EN 3527:2025

Active Most Recent

Aerospace series. Steel 33CrMoV12 (1.8522). Air melted. Softened. Forging stock. a or D = 300 mm

€172.00

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BS EN 3365:2025

BS EN 3365:2025

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Aerospace series. Steel X15CrNi17-3 (1.4057). Air melted. Softened. Forging stock. a or D = 300 mm

€172.00

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BS EN 3359:2025

BS EN 3359:2025

Active Most Recent

Aerospace series. Steel X3CrNiMoAl13-8-2 (1.4534). Vacuum induction melted and consumable electrode remelted. Softened. Forging stocks. a or D = 300 mm

€172.00

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BS EN 3490:2025

BS EN 3490:2025

Active Most Recent

Aerospace series. Steel X15CrNi17-3 (1.4057). Air melted. Hardened and tempered. Bars for machining. De = 200 mm. 900 MPa = Rm = 1 100 MPa

€172.00

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BS EN 3531:2025

BS EN 3531:2025

Active Most Recent

Aerospace series. Steel X2NiCoMo18-8-5 (1.6359). Vacuum induction melted and vacuum arc remelted. Solution treated and precipitation treated. Sheets and strips. a ? 6 mm. 1750 MPa ? Rm ? 2 000 MPa

€172.00

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BS EN 3532:2025

BS EN 3532:2025

Active Most Recent

Aerospace series. Steel X2NiCoMo18-8-5 (1.6359). Vacuum induction melted and vacuum arc remelted. Solution treated and precipitation treated. Plates. 6 mm < a = 40 mm. 1 750 MPa = Rm = 2 000 MPa

€172.00

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ASTM A989/A989M-25

ASTM A989/A989M-25

Active Most Recent

Standard Specification for Hot Isostatically-Pressed Alloy Steel Flanges, Fittings, Valves, and Parts for High Temperature Service

€65.00

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ISO 16691:2014 (R2023)

ISO 16691:2014 (R2023)

Active Most Recent

Space systems — Thermal control coatings for spacecraft — General requirements

€113.00

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ISO/TS 16697:2012 (R2022)

ISO/TS 16697:2012 (R2022)

Superseded Historical

Space systems — Safety and compatibility of materials - Method to determine the flammability thresholds of materials

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

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ISO 14624-5:2023

ISO 14624-5:2023

Active Most Recent

Space systems — Safety and compatibility of materials

€75.00

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SAE AMS 1384A:2007-02-16

SAE AMS 1384A:2007-02-16

Superseded Historical

ACID, INHIBITED PHOSPHORIC Aircraft Turbine Engine Components Room Temperature Application

€75.00

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SAE AMS 2253D:1983-01-01

SAE AMS 2253D:1983-01-01

Superseded Historical

Tolerances Carbon and Alloy Steel Tubing

€67.00

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SAE AMS 6520D:2011-11-03

SAE AMS 6520D:2011-11-03

Superseded Historical

Steel, Maraging, Sheet, Strip, and Plate 18Ni - 7.8Co - 4.9Mo - 0.40Ti - 0.10Al Consumable Electrode Melted, Solution Heat Treated

€68.00

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SAE AMS 7267G:2001-04-01

SAE AMS 7267G:2001-04-01

Superseded Historical

Rings, Sealing, Silicone (VSI) Rubber Heat-Resistant, Low Compression Set 70 - 80

€77.00

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