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Last Updated: April 11, 2026

Maraging steels, useable in ‘missiles’, having all of the following: N.B.: SEE ALSO 1C216.

Code

1C116

EU Code

M6C8

Categories
  • ANNEX II - List of other goods and technology, including software, referred to in Article 3a
  • ANNEX III - CATEGORY 1 — SPECIAL MATERIALS AND RELATED EQUIPMENT
Subcategory

A1. aterials, chemicals, ‘microorganisms’ and ‘toxins’

Prohibited Supply To
IR
Authority
EU
Document

EU Regulation No 267/2012

Note

Maraging steels, usable in the systems specified in 1.A. or 19.A.1., having all of the following: a. Having an ultimate tensile strength, measured at 20 °C, equal to or greater than: 1. 0,9 GPa in the solution annealed stage; or 2. 1,5 GPa in the precipitation hardened stage; and b. Any of the following forms: 1. Sheet, plate or tubing with a wall or plate thickness equal to or less than 5,0 mm; or 2. Tubular forms with a wall thickness equal to or less than 50 mm and having an inner diameter equal to or greater than 270 mm. Technical Note: Maraging steels are iron alloys: a. Generally characterised by high nickel, very low carbon content and use substitutional elements or precipitates to produce strengthening and agehardening of the alloy; and b. Subjected to heat treatment cycles to facilitate the martensitic transformation process (solution annealed stage) and subsequently age hardened (precipitation hardened stage).

Program information
Program information

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