DI-MC 355 B (EN S355M)

Alternative and trade names
EN 10025-4 Grade S355M
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Description

DI-MC 355 is a thermomechanically rolled, fine grained structural steel with minimum yield strength of 355 MPa in its delivery condition ex works (referring to the lowest thickness range). It fulfils the requirements of EN 10025-4.

Due to its chemical composition, this material has a low carbon equivalent and hence excellent weldability. The steel is preferentially used by the customers in constructional steelwork, hydraulic steelwork and mechanical engineering, where exacting demands are placed on weldability.

Related Standards

Equivalent Materials

This material data has been provided by Dillinger.

"Typical" values were obtained via a literature search. "Predicted" values were imputed via artificial intelligence technology. While we have placed significant efforts in ensuring data accuracy, "typical" and "predicted" data should be considered indicative and verified by appropriate material testing. Please do contact us if additional information on the the predicted data method is required.
All metrics apply to room temperature unless otherwise stated. SI units used unless otherwise stated.
Equivalent standards are similar to one or more standards provided by the supplier. Some equivalent standards may be stricter whereas others may be outside the bounds of the original standard.

Ashby charts

Properties

General

PropertyValueComment

Carbon equivalent (CET)

0.21 [-]

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typ. value for thickness 40 < t < 80 mm

0.22 [-]

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typ. value for thickness 80 ≤ t ≤ 120 mm

0.23 [-]

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for thickness 120 < t ≤ 150 mm

0.24 [-]

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typ. value for thickness 8 ≤ t ≤ 40 mm

Carbon equivalent (CEV)

0.33 [-]

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typ. value for thickness 40 < t ≤ 120 mm

0.34 [-]

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typ. value for thickness 8 ≤ t ≤ 16 mm

0.34 [-]

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max. value for thickness 40 < t ≤ 63 mm

0.35 [-]

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typ. value for thickness 16 < t ≤ 40 mm

0.35 [-]

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max. value for thickness 63 < t ≤ 120 mm

0.36 [-]

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max. value for thickness 8 ≤ t ≤ 16 mm

0.37 [-]

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max. value for thickness 16 < t ≤ 40 mm

0.38 [-]

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typ. value for thickness 120 < t ≤ 150 mm

0.39 [-]

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max. value for thickness 8 ≤ t ≤ 40 mm according to EN 10025-4

0.4 [-]

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max. value for thickness 40 < t ≤ 63 mm according to EN 10025-4

0.4 [-]

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max. value for thickness 120 < t ≤ 150 mm

0.45 [-]

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max. value for thickness 63 < t ≤ 150 mm according to EN 10025-4

Carbon equivalent note

CEV = C + Mn/6 + (Cr+Mo+V)/5 + (Cu+Ni)/15 and CET = C + (Mn+Mo)/10 + (Cr+Cu)/20 + Ni/40

Mechanical

PropertyTemperatureValueComment

Charpy impact energy, V-notch

-20 °C

20 J

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average of 3 tests | longitudinal/transverse specimens

-20 °C

40 J

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average of 3 tests | longitudinal/transverse specimens

-10 °C

24 J

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average of 3 tests | longitudinal/transverse specimens

-10 °C

43 J

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average of 3 tests | longitudinal/transverse specimens

0 °C

27 J

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average of 3 tests | longitudinal/transverse specimens

0 °C

47 J

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average of 3 tests | longitudinal/transverse specimens

Elongation

22 %

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min. for plate thickness t ≤ 150 | transverse specimens, A5

Tensile strength

430 - 590 MPa

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for plate thickness 100 < t ≤ 150 mm | transverse specimens

440 - 600 MPa

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for plate thickness 63 < t ≤ 100 mm | transverse specimens

450 - 610 MPa

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for plate thickness 40 < t ≤ 63 mm | transverse specimens

470 - 630 MPa

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for plate thickness t ≤ 40 mm | transverse specimens

Yield strength

320 MPa

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min. ReH for plate thickness 100 < t ≤ 150 mm | transverse specimens

325 MPa

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min. ReH for plate thickness 63 < t ≤ 100 mm | transverse specimens

335 MPa

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min. ReH for plate thickness 40 < t ≤ 63 mm | transverse specimens

345 MPa

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min. ReH for plate thickness 16 < t ≤ 40 mm | transverse specimens

355 MPa

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min. ReH for plate thickness t ≤ 16 mm | transverse specimens

Chemical properties

PropertyValueComment

Aluminium

0.02 %

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min.

Carbon

0.13 %

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max.

Chromium

0.3 %

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max.

Copper

0.4 %

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max.

Iron

Balance

Manganese

1.6 %

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max.

Molybdenum

0.1 %

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max.

Nickel

0.5 %

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max.

Niobium

0.05 %

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max.

Nitrogen

0.01 %

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max.

Phosphorus

0.02 %

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max.

Silicon

0.5 %

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max.

Sulfur

0.003 %

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max.

Titanium

0.02 %

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max.

Vanadium

0.08 %

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max.

Technological properties

Property
Cold Forming

With regard to its high toughness, DI-MC 355 can generally be well cold formed, i.e. at temperatures below 580 °C. Cold forming is always related to a hardening of the steel and to a decrease in ductility. This change in the mechanical properties can in general be partially recovered through a subsequent stress relief heat treatment. Flame cut or sheared edges in the bending area should be ground before cold forming. For larger cold forming degrees we recommend consulting us before ordering.

Delivery condtion

DI-MC 355 can be delivered in two qualities as follows:

  • Basic quality (B) with minimum impact values at –20 °C: DI-MC 355 B Applicable in the sense of S355M in accordance with EN 10025-4
  • Low temperature quality (T) with minimum impact values at –50 °C: DI-MC 355 T Applicable in the sense of S355ML in accordance with EN 10025-4.

    DI-MC 355 can be delivered in thickness from 8 to 150 mm according to the dimensional programme.

    For DI-MC 355, under the designations DI-MC 355 B/S355M and DI-MC 355 T/S355ML, a CE-marking is applied in thicknesses up to 150 mm, unless otherwise agreed.

    For DI-MC 355, under the designations DI-MC 355 B/S355M and DI-MC 355 T/S355ML, the „marque NFAcier“ can be applied, if agreed.


    Unless otherwise agreed, the general technical delivery requirements in accordance with EN 10021 apply.

  • Flame cutting and welding

    DI-MC 355 can be flame cut in all thickness ranges without preheating. Plasma and laser cutting can also be carried out without preheating for typical thickness.

    DI-MC 355 has an excellent weldability if the general technical rules are observed (EN 1011 has to be applied analogously). The risk of cold cracking is low, so that preheating is often not necessary when welding. With greater plate thicknesses, omitting the preheating requires the use of filler materials and welding conditions that lead to a very low hydrogen transfer (up to 5 ml/100 g DM according to ISO 6390).

    The low content of carbon and other alloy elements leads to favourable toughness properties in the heat affected zone, even with high heat inputs. Depending on the chosen welding process, welding filler material as well as toughness requirements in the heat affected zone, it permits cooling temperatures (t8/5) above the limiting values of 25 s as stated in EN 1011-2 and SEW 088.

    Flame straightening

    For flame straightening, working recommendations are given in the “DI-MC Processing instructions Flame straightening”. For thermomechanically rolled steel the report CEN/TR 10347 recommends the same maximum flame straightening temperature as for normalized steel.

    General note

    If special requirements which are not covered in this material data sheet are to be met by the steel due to its intended use or processing, these requirements are to be agreed before placing the order.

    The information in this data sheet is a product description. This data sheet is updated at irregular intervals. The current version is relevant. The current version is available from the mill or as download at www.dillinger.de.

    Heat Treatment

    Welded joints of DI-MC 355 are usually used in welded condition. If a stress relief heat treatment is necessary, it is carried out in the temperature range between 530 and 580 °C with cooling in air. The holding time should not exceed 4 hours (even if multiple operations are carried out). For particular heat treatment requirements we recommend consulting us before ordering.

    Hot forming

    Hot forming, i.e. forming at temperatures above 580 °C, leads to changes in the original material condition. It is impossible to re-establish the same material properties that had been achieved during the original manufacture through a further heat treatment. Therefore hot forming is not permitted.

    Options

    Optionally it is possible to order DI-MC 355 in the whole thickness range (up to 150 mm) with a minimum yield strength of 355 MPa, as well as a tensile strength range of 470 MPa (see option 1).


    Options:

    1) Yield strength of 355 MPa, as well as a tensile strength range of 470 MPa independent of plate thickness.

    2) The impact properties and the tensile properties shall be verified for each mother plate

    Other

    Identification: Unless otherwise agreed, the marking is carried out via steel stamps with at least the following information:

  • The steel designation (DI MC355B S355M or DI MC355T S355ML)
  • The heat number
  • The number of mother plate and individual plate
  • The manufacturer’s sign
  • The inspection representative’s sign

  • Processing methods

    The entire processing and application techniques are of fundamental importance to the reliability of the parts and assemblies made from this steel. The user should ensure that his design, construction and processing methods are aligned with the material, correspond to the state-of-the-art that the fabricator has to comply with and are suitable for the intended use. The customer is responsible for the selection of the material. The recommendations in accordance with EN 1011 and SEW 088 should be observed. You find detailed information on processing in the “DI-MC Processing instructions”.

    Surface condition

    Unless otherwise agreed, the specifications will be in accordance with EN 10163, class A2

    Testings

    Tensile test and impact tests are carried out once per heat, 60 t and thickness range as specified for the yield strength according to table 5 of EN 10025-4. Tests on every mother plate are possible on request (see option 2).

    The test pieces are taken and prepared according to parts 1 and 4 of EN 10025.

    The tensile test is carried out on specimens of gauge length Lo = 5.65⋅√So respectively Lo = 5⋅do, in accordance with EN ISO 6892-1. The impact test will be carried out on Charpy-V-specimens in accordance with

    EN ISO 148-1 using a 2 mm striker. Unless otherwise agreed, the test will be performed according to

    EN ISO 148-1 on longitudinal test pieces at a temperature of -20 °C for the basic quality B and at -50 °C for the low temperature quality T.

    Unless otherwise agreed, the test results are documented in a certificate 3.1 in accordance with EN 10204.

    Unless otherwise agreed, DI-MC 355 meets the requirements of class S1E1 in accordance with EN 10160.

    Tolerances

    Unless otherwise agreed, tolerances are in accordance with 10029, with class A for the thickness.