Gyros or angular rate sensors, having any of the following and specially designed components therefor: (a) Specified to function at linear acceleration levels less than or equal to 100 g and having any of the following: 1. A rate range of less than 500 degrees per second and having any of the following: a. A ‘bias’‘stability’ of less (better) than 0,5 degree per hour, when measured in a 1 g environment over a period of one month, and with respect to a fixed calibration value; or b. An ‘angle random walk’ of less (better) than or equal to 0,0035 degree per square root hour; or Note : this paragraph does not apply to ‘spinning mass gyros’. 2. A rate range greater than or equal to 500 degrees per second and having any of the following: a. A ‘bias’‘stability’ of less (better) than 4 degrees per hour, when measured in a 1 g environment over a period of three minutes, and with respect to a fixed calibration value; or b. An ‘angle random walk’ of less (better) than or equal to 0,1 degree per square root hour; or Note : this paragraph does not apply to ‘spinning mass gyros’. (b) Specified to function at linear acceleration levels exceeding 100 g.
Code
7A002
EU Code
VII.A7.002
Category
ANNEX III - CATEGORY 7 — NAVIGATION AND AVIONICS
Subcategory
7A - Systems, Equipment and Components
Prohibited Supply To
Iran
Authority
EU
Document
EU Regulation No 267/2012
Note
Accelerometers or gyros of any type, designed for use in inertial navigation systems or in guidance systems of all types, specified to function at acceleration levels greater than 100 g, and specially designed components therefor.Note:9.A.5. does not include accelerometers that are designed to measure vibration or shock.