49.025.99 - Other materials
ICS 49.025.99 Details
Other materials
Weitere Materialien der Luft- und Raumfahrttechnik
Autres materiaux
Drugi materiali
General Information
e-Library Subscription
Create subscription and get permanent access to documents within 49.025.99 - Other materials
Currently subscription includes documents marked with .We are working on making all documents available within the subscription.
This document specifies the requirements for hexavalent chromium free anodizing of aluminium and aluminium alloys for corrosion protection, bonding and painting.
This document does not apply to hard anodizing and plasma electrolytic anodizing (micro-arc oxidation).
The purpose of this document is to give design, quality and manufacturing requirements. It does not give complete in-house process instructions; these are given in the processor's detailed process instructions.
- Standard33 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the requirements relating to:
Heat-resisting alloy NI-PH1301 (NiCr19Co18Mo4Ti3Al3)
Solution treated and precipitation treated
Bars and sections
De ≤ 200 mm
for aerospace applications.
- Standard9 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the requirements relating to:
Heat-resisting alloy NI-PH1301 (NiCr19Co18Mo4Ti3Al3)
Solution treated and precipitation treated
Bars and sections
De ≤ 200 mm
for aerospace applications.
- Standard9 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the general organization of the EN standards for non-metallic materials and their links with other types of standards for aerospace applications.
It corresponds to level 0 (see 4.1).
- Standard8 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the general rules for drafting and presentation of EN aerospace series non-metallic material technical specifications.
- Standard21 pagesEnglish languagesale 10% offe-Library read for1 day
The scope includes metallic Powder Bed Fusion technologies for space applications.
A clear definition and implementation of quality monitoring and control means is mandatory and shall address the full end to end metallic PBF process, encompassing:
- Design / Simulation
- Materials management (Powder, shielding gases, other consumables, recycling, etc.)
- Processing
- Post Processing
- Testing
By developing a single standard which can be tailored in the Project definition phase, it will help the Space Industry in performing the following functions
related to metallic PBF technologies over the full end to end process:
(i) select and qualify metallic PBF processes for the appropriate application,
(ii) select and validate raw materials for the appropriate applications,
(iii) define monitoring and control means during production to ensure that metallic PBF parts are produced with the required quality,
(iv) define requirements for applying Non-Destructive Inspection methods for the different metallic PBF parts,
(v) define requirements to verify/qualify space parts produced by metallic PBF processes for the selected applications and associated environment,
(vi) define specific requirements for operators/inspectors/instructors certification,
(vii) define requirements for metallic PBF machines certification,
(viii) define requirements for metallic PBF Companies certification.
The Standard will be complemented with informative Annexes, listing guidelines and best practices on specific technical aspects.
- Standard78 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the requirements for a range of one part anaerobic polymerisable compounds
which polymerises upon the exclusion of oxygen and activation by a metal surface.
- Standard17 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the general organization of the EN standards for non-metallic materials and their links with other types of standards for aerospace applications.
It corresponds to level 0 (see 4.1).
- Standard8 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the method for depositing cadmium layers according to the vacuum deposition
process, for use in aerospace construction.
According to this process, cadmium metal is vaporized under vacuum and deposited directly on the
base material with an interlayer. The coating produced in this way is ductile and electrically conductive.
This document is applicable whenever referenced.
- Standard15 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the general rules for drafting and presentation of EN aerospace series non-metallic material technical specifications.
- Standard21 pagesEnglish languagesale 10% offe-Library read for1 day
The scope includes metallic Powder Bed Fusion technologies for space applications.
A clear definition and implementation of quality monitoring and control means is mandatory and shall address the full end to end metallic PBF process, encompassing:
• Design / Simulation
• Materials management (Powder, shielding gases, other consumables, recycling, etc.)
• Processing
• Post Processing
• Testing
By developing a single standard which can be tailored in the Project definition phase, it will help the Space Industry in performing the following functions
related to metallic PBF technologies over the full end to end process:
(i) select and qualify metallic PBF processes for the appropriate application,
(ii) select and validate raw materials for the appropriate applications,
(iii) define monitoring and control means during production to ensure that metallic PBF parts are produced with the required quality,
(iv) define requirements for applying Non-Destructive Inspection methods for the different metallic PBF parts,
(v) define requirements to verify/qualify space parts produced by metallic PBF processes for the selected applications and associated environment,
(vi) define specific requirements for operators/inspectors/instructors certification,
(vii) define requirements for metallic PBF machines certification,
(viii) define requirements for metallic PBF Companies certification.
The Standard will be complemented with informative Annexes, listing guidelines and best practices on specific technical aspects.
- Standard78 pagesEnglish languagesale 10% offe-Library read for1 day
This document provides a list of terms with their definitions illustrated by typical photographs, in order
to define a common vocabulary on the imperfections and damage that may occur during the
manufacture of organic matrix composite materials (which will be called “resin” in this document).
Some types of damage may also be encountered in use.
This document is restricted to their definitions and does not give any acceptance criteria. The word
“imperfection” will be preferred to the word “defect”, although the word “defect” might be usually used.
Defect acceptance criteria to be discussed between the user and customer and documented
appropriately between the two parties.
- Standard54 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the requirements relating to:
Heat resisting nickel base alloy (NI-P101HT)
Cold worked and solution treated
Bars for machining for fasteners
3 mm ≤ D ≤ 50 mm
for aerospace applications.
- Standard8 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the requirements relating to:
Heat resisting alloy FE-PM1708
Vacuum arc remelted
As forged
Forging stock
De ≤ 300 mm
for aerospace applications.
- Standard8 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the requirements relating to:
Heat resisting alloy FE-PM1708
Vacuum arc remelted
Hardened and tempered
Bars
a or D ≤ 200 mm
1 000 MPa ≤ Rm ≤ 1 140 MPa
for aerospace applications.
- Standard8 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the requirements relating to:
Heat resisting nickel base alloy (NI-P100HT)
Cold worked and softened
Bar and wire for continuous forging or extrusion for fasteners
3 mm ≤ D ≤ 30 mm
- Standard8 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the requirements relating to:
Heat resisting alloy NI-PH2601
Solution treated and cold worked
Bar for forged fasteners
D ≤ 50 mm
1 550 MPa ≤ Rm ≤ 1 830 MPa
for aerospace applications.
- Standard8 pagesEnglish languagesale 10% offe-Library read for1 day
EN 4244 specifies the requirements relating to:Heat resisting alloy FE-PM1708 Vacuum arc remelted Hardened and tempered Bars a or D ≤ 200 mm 1 000 MPa ≤ Rm ≤ 1 140 MPa
- Standard8 pagesEnglish languagesale 10% offe-Library read for1 day
This European Standard specifies the requirements relating to:
Heat resisting nickel base alloy (Ni-P101HT)
Cold worked and solution treated
Bar for machining for fasteners
3 mm ≤ D ≤ 50 mm
for aerospace applications.
- Standard8 pagesEnglish languagesale 10% offe-Library read for1 day
This document is part of the series of EN metallic material standards for aerospace applications. The general organization of this series is described in EN 4258.
This document has been prepared in accordance with EN 4500-003.
- Standard8 pagesEnglish languagesale 10% offe-Library read for1 day
This document defines the requirements for the preparation of forged test samples.
Unless otherwise specified on the drawing, order, or inspection schedule, this document shall be applied when referenced in the relevant EN material standard or EN technical specification.
This document applies to round products of ≥ 20 mm diameters or other shapes of equivalent cross-section.
- Standard7 pagesEnglish languagesale 10% offe-Library read for1 day
This standard specifies the requirements relating to:Heat resisting nickel base alloy (NI-P100HT)Cold worked and softenedBar and wire for continuous forging or extrusion for fasteners3 mm ≤ D ≤ 30 mmfor aerospace applications.
- Standard8 pagesEnglish languagesale 10% offe-Library read for1 day
This standard specifies the requirements relating to: Heat resisting alloy NI-PH 2601Solution treated and cold worked Bar for forged fasteners D ≤ 50 mm1 550 MPa ≤ Rm ≤ 1 830 MPa.
- Standard8 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the requirements relating to:
Heat resisting alloy NI-PH1302 (NiCr20Co13Mo4Ti3Al)
Solution treated and cold worked
Bar for forged fasteners
3 mm ≤ D ≤ 30 mm
for aerospace applications.
- Standard8 pagesEnglish languagesale 10% offe-Library read for1 day
This European Standard defines the requirements for the preparation of forged test samples. Unless otherwise specified on the drawing, order, or inspection schedule, this document shall be applied when referenced in the relevant EN material standard or EN technical specification. This document applies to round products of ≥ 20 mm diameters or other shapes of equivalent cross-section.
- Standard7 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the requirements relating to:
Heat resisting nickel base alloy (Ni-P101HT)
Cold worked and softened
Bar and wire for continuous forging or extrusion for fasteners
3 mm ≤ D ≤ 30 mm
for aerospace applications.
- Standard8 pagesEnglish languagesale 10% offe-Library read for1 day
This European Standard specifies the requirements relating to:
Heat resisting alloy NI-PH2601
Solution treated and cold worked
Bar for forged fasteners
D ≤ 50 mm
1 270 MPa ≤ Rm ≤ 1 550 MPa
for aerospace applications.
- Standard8 pagesEnglish languagesale 10% offe-Library read for1 day
This European Standard specifies two methods for the determination of the application time of sealants.
- Standard6 pagesEnglish languagesale 10% offe-Library read for1 day
This European Standard specifies two methods for the determination of the application time of sealants.
- Standard6 pagesEnglish languagesale 10% offe-Library read for1 day
This standard specifies the requirements for glass fabric/phenolic resin preimpregnates. It shall be used together with EN 2833-1.
- Standard9 pagesEnglish languagesale 10% offe-Library read for1 day
This European Standard describes the preparation of panels with any desired fibre orientation of unidirectional orientated carbon fibre or fabric with thermosetting resins. The purpose of this standard is to describe recommended processes for the preparation of the panels from which test specimens subsequently are machined. Standard specimens prepared in this manner may be used either for evaluating the components i.e. the carbon reinforcement, finishes, resins, catalysts, curing agents, etc. or for verifying the overall quality of the finished products.
- Standard11 pagesEnglish languagesale 10% offe-Library read for1 day
This European Standard defines the requirements for the determination of the modulus of rupture of glass transparencies for aircraft applications, whether in the annealed or chemically or thermally tempered condition.
- Standard9 pagesEnglish languagesale 10% offe-Library read for1 day
This European Standard defines the requirements for the determination of the flatness of monolithic glass transparencies for aircraft applications. The method is designed to eliminate the effect of the glass deflecting under its own weight, thus eliminating false results.
- Standard9 pagesEnglish languagesale 10% offe-Library read for1 day
This European Standard specifies the requirements relating to universally available and high light transmission, chemically tempered float glass plies, for aerospace applications.
- Standard8 pagesEnglish languagesale 10% offe-Library read for1 day
This European Standard specifies the requirements relating to universally available and high light transmission, thermally tempered float glass plies, for aerospace applications.
- Standard8 pagesEnglish languagesale 10% offe-Library read for1 day
This European Standard defines a qualitative method for the determination of the ream and surface ripple in glass transparencies for aircraft applications.
- Standard7 pagesEnglish languagesale 10% offe-Library read for1 day
This European Standard defines the requirements for the determination of the modulus of rupture of glass transparencies for aircraft applications, whether in the annealed or chemically or thermally tempered condition.
- Standard9 pagesEnglish languagesale 10% offe-Library read for1 day
This European Standard defines the test method for the determination of the operability of a cured sealant during and after submission to a bending load at low temperatures (low-temperature flexibility).
- Standard7 pagesEnglish languagesale 10% offe-Library read for1 day
This European Standard defines the requirements for the determination of the flatness of monolithic glass transparencies for aircraft applications. The method is designed to eliminate the effect of the glass deflecting under its own weight, thus eliminating false results.
- Standard9 pagesEnglish languagesale 10% offe-Library read for1 day
This European Standard defines a qualitative method for the determination of the ream and surface ripple in glass transparencies for aircraft applications.
- Standard7 pagesEnglish languagesale 10% offe-Library read for1 day
This European Standard specifies the requirements relating to universally available and high light transmission, thermally tempered float glass plies, for aerospace applications.
- Standard8 pagesEnglish languagesale 10% offe-Library read for1 day
This European Standard specifies the requirements relating to universally available and high light transmission, chemically tempered float glass plies, for aerospace applications.
- Standard8 pagesEnglish languagesale 10% offe-Library read for1 day
This European Standard defines the test method for the determination of the operability of a cured sealant during and after submission to a bending load at low temperatures (low-temperature flexibility).
- Standard7 pagesEnglish languagesale 10% offe-Library read for1 day
This standard defines the test equipment, apparatus and media required for determination of the smoke density according to EN 2825 and the concentration of the gas components in the smoke according to EN 2826 due to pyrolitic decomposition of solid materials and composite materials of up to 25 mm in thickness under the influence of radiant heat only or with simultaneous flame application.
This test method applies exclusively to materials whose specific standard requires this type of test. It cannot be substituted for the statutory tests required for a final specific use of the material concerned.
NOTE The smoke gas density and the gas components in the smoke are determined according to the specific environmental and test conditions defined in this standard, in EN 2825 and EN 2826. No studies have been made up to now to determine whether the results can be transferred to differing conditions, particularly to actual fire conditions. The inhalatory toxical risk and irritancy affect cannot be assessed by merely measuring the concentration of individual gas components in the smoke.
- Standard18 pagesEnglish languagesale 10% offe-Library read for1 day
This European Standard defines a test method for determination of the smoke density due to pyrolitic decomposition of solid materials and composite materials of up to 25 mm in thickness under the influence of radiant heat only or with simultaneous flame application.
The test results enable a comparison of the smoke production of different materials or material configurations under the conditions specified in this standard.
NOTE 1 The smoke gas density is determined according to the specific environmental and test conditions defined in EN 2824 and this standard. No studies have been made up to now to determine whether the results can be transferred to differing conditions, particularly to actual fire conditions.
NOTE 2 The burning behaviour - and consequently the smoke density - of aerospace materials are not only influenced by the type of material but also to a large extent by the configuration, the specific surface and mass, the combination with other materials, the means of joining as well as the processing technique.
- Standard9 pagesEnglish languagesale 10% offe-Library read for1 day
This European Standard defines a test method to determine the concentration of certain gas components due to pyrolitic decomposition of solid materials and composite materials under the influence of radiant heat only or with simultaneous flame application.
NOTE 1 The gas components in the smoke are determined according to the specific environmental and test conditions defined in EN 2824 and this standard. No studies have been made up to now to determine whether the results can be transferred to different conditions, particularly to actual fire conditions. The inhalatory toxical risk and irritancy affect cannot be assessed by merely measuring the concentration of individual gas components in the smoke.
NOTE 2 The burning behaviour and consequently the gas components in the smoke of aerospace materials are not only influenced by the type of material but also to a large extent by the configuration, the specific surface and mass, the combination with other materials, the means of joining as well as the processing technique.
NOTE 3 These influences shall be taken into account in the preparation of tests, the selection of test specimens and the interpretation of test results.
- Standard10 pagesEnglish languagesale 10% offe-Library read for1 day
This standard specifies the requirements relating to:
Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb)
Non heat treated
Forging stock
a or D £ 250 mm
for aerospace applications.
- Standard6 pagesEnglish languagesale 10% offe-Library read for1 day
This standard specifies the requirements relating to:
Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb)
Solution treated
Seamless tubes
For hydraulic application
D ≤ 50 mm, a≤ 3 mm
for aerospace applications.
- Standard6 pagesEnglish languagesale 10% offe-Library read for1 day
This standard specifies the requirements relating to:
Heat resisting alloy NI-CH2601 (NiCr19Fe19Nb5Mo3)
Non heat treated
Remelting stock
for aerospace applications.
- Standard6 pagesEnglish languagesale 10% offe-Library read for1 day
This standard specifies the requirements relating to:
Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb)
Non heat treated
Forging stock
a or D £ 250 mm
for aerospace applications.
- Standard6 pagesEnglish languagesale 10% offe-Library read for1 day