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Last Updated: April 11, 2026

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Last Updated: April 11, 2026

Good

‘Compensation systems’ for the following: (a) ‘Magnetometers’ using optically pumped or nuclear precession (proton/ Overhauser) ‘technology’ having a ‘sensitivity’ lower (better) than 20 pT (rms) per square root Hz at a frequency of 1 Hz, and using optically pumped or nuclear precession (proton/Overhauser) ‘technology’ that will permit these sensors to realize a ‘sensitivity’ lower (better) than 2 pT rms per square root Hz. (b) Underwater electric field sensors having a ‘sensitivity’ lower (better) than 8 nanovolt per meter per square root Hz when measured at 1 Hz. (c) ‘Magnetic gradiometers’ specified in VII.A6.010 that will permit these sensors to realize a ‘sensitivity’ lower (better) than 3 pT/m rms per square root H Note: Fibre optic ‘intrinsic magnetic gradiometers’ having a magnetic gradient field ‘sensitivity’ lower (better) than 0,3 nT/m (rms) per square root Hz; ‘Intrinsic magnetic gradiometers’, using ‘technology’ other than fibre-optic ‘technology’, having a magnetic gradient field ‘sensitivity’ lower (better) than 0,015 nT/m (rms) per square root Hz.

Code

6A006

EU Code

VII.A6.011

Category

ANNEX III - CATEGORY 6 — SENSORS AND LASERS

Subcategory

6A - Systems, Equipment and Components

Prohibited Supply To
IR
Authority
EU
Document

EU Regulation No 267/2012

Note

Three axis magnetic heading sensors having all of the following characteristics, and specially designed components therefor: a) Internal tilt compensation in pitch (+/– 90 degrees) and having roll (+/– 180 degrees) axes. b) Capable of providing azimuthal accuracy better (less) than 0,5 degrees rms at latitudes of +/– 80 degrees, referenced to local magnetic field; and c) Designed or modified to be integrated with flight control and navigation systems. Note: Flight control and navigation systems in Item 9.A.8. include gyrostabilisers, automatic pilots and inertial navigation systems.

Program information
Program information

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