6D102
"Software" specially designed or modified for the "use" of goods specified in I.6A.005.
I.6B.002
6D103
"Software" which processes post-flight, recorded data, enabling determination of vehicle position throughout its flight path, specially designed or modified for 'missiles'.
Technical Note:
In I.6B.002 'missile' means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.
I.6B.003
ex 6E001
"Technology" according to the General Technology Note for the "development" of equipment, materials or "software" specified in I.6A.001, I.6A.002.c, I.6A.003, I.6A.004 to I.6A.010, I.6B.001 or I.6B.002.
I.6B.004
ex 6E002
"Technology" according to the General Technology Note for the "production" of equipment or materials specified in I.6A.001, I.6A.002.c or I.6A.003 to I.6A.010.
I.6B.005
ex 6E101
"Technology" according to the General Technology Note for the "use" of equipment or "software" specified in I.6A.002 to I.6A.005, I.6A.011, I.6B.001 or I.6B.002.
I.6B.006
ex 6E201
"Technology" according to the General Technology Note for the "use" of equipment specified in I.6A.001 or I.6A.006 to I.6A.010.
I.7
NAVIGATION AND AVIONICS
I.7A Goods
No
Relevant item(s) from Annex to Regulation (EC) No 1183/2007
Description
I.7A.001
ex 7A002*
(ex 7A002.a and ex 7A002.d)
Gyros having any of the following characteristics, and specially designed components therefor:
N.B.: See also I.7A.003.
a.
A "drift rate""stability", when measured in a 1 g environment over a period of one month and with respect to a fixed calibration value, of less (better) than 0,5 degree per hour when specified to function at linear acceleration levels up to and including 100 g; or
d.
Specified to function at linear acceleration levels exceeding 100 g.
I.7A.002
7A101, ex 7A001.a.3
Accelerometers as follows, and specially designed components therefor:
a.
Linear accelerometers, designed for use in inertial navigation systems or in guidance systems of all types, usable in 'missiles', having all the following characteristics, and specially designed components therefor;
1.
A "bias""repeatability" of less (better) than 1 250 micro g; and
2.
A "scale factor""repeatability" of less (better) than 1 250 ppm;
Note: I.7A.002.a. does not specify accelerometers which are specially designed and developed as MWD (Measurement While Drilling) Sensors for use in downhole well service operations.
1.
In I.7A.002.a. 'missile' means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km;
2.
In I.7A.002.a. the measurement of "bias" and "scale factor" refers to a one sigma standard deviation with respect to a fixed calibration over a period of one year;
b.
Continuous output accelerometers specified to function at acceleration levels exceeding 100 g.
I.7A.003
7A102*
All types of gyros other than those specified in I.7A.001, usable in 'missiles', with a rated "drift rate""stability" of less than 0,5 ° (1 sigma or rms) per hour in a 1 g environment and specially designed components therefor.
Technical Note:
In I.7A.003 'missile' means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.
I.7A.004
ex 7A103
(7A103.a, ex 7A103.b and 7A103.c)
Instrumentation, navigation equipment and systems, as follows; and specially designed components therefor:
a.*
Inertial or other equipment using