parts” and “components” therefor
The list of items controlled is contained in theECCN heading.
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7A005 Global Navigation Satellite Systems (GNSS) receiving equipment having any of the following (see List of Items Controlled) and “specially designed” “components”
therefor.
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a. Employing a decryption algorithm “specially designed” or modified for government use to access the ranging code for position and time; or
b. Employing ‘adaptive antenna systems’.
Note: 7A005.b does not apply to GNSS receiving equipment that only uses “components” designed to filter, switch, or combine signals from multiple omni-directional
antennas that do not implement adaptive antenna techniques.
Technical Note: For the purposes of 7A005.b ‘adaptive antenna systems’ dynamically generate one or more spatial nulls in an antenna array pattern by signal processing in the time domain or frequency domain.
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7A105 Receiving equipment for Global Navigation Satellite Systems (GNSS) (e.g. GPS, GLONASS, or Galileo)
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1. Designed or modified for use in “missiles”;
or
2. Designed or modified for airborne
applications and having any of the following:
2.a. Capable of providing navigation information at speeds in excess of 600 m/s (1,165 nautical mph);
2.b. Employing decryption, designed or modified for military or governmental services, to gain access to GNSS secured signal/data; or
2.c. Being “specially designed” to employ anti-jam features (e.g. null steering antenna or electronically steerable antenna) to function in an environment of active or passive countermeasures
.
Note to 7A105: See also 7A005 and 7A994
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7A006 Airborne altimeters operating at frequencies other than 4.2 to 4.4 GHz inclusive and having any of the following
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a. “Power management”; or
b. Using phase shift key modulation.
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7A106 Altimeters, other than those controlled by 7A006, of radar or laser radar type, designed or modified for use in “missiles”.
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a. Internal tilt compensation in pitch (+/-90 degrees) and 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 7A107 include gyrostabilizers, automatic pilots and inertial navigation systems.
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7A008 Underwater sonar navigation systems using Doppler velocity or correlation velocity logs integrated with a heading
source and having a positioning accuracy of
equal to or less (better) than 3% of distance
traveled “Circular Error Probable” (“CEP”)
and “specially designed” “components
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The list of items controlled is contained in the ECCN heading.
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7A115 Passive sensors for determining bearing to specific electromagnetic sources (direction finding equipment) or terrain characteristics, designed or modified for use in “missiles”.
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(These items are “subject to the ITAR”. See 22 CFR parts 120 through 130.)
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7A116 Flight control systems (hydraulic,
mechanical, electro-optical, or electromechanical flight control systems (including
fly-by-wire systems) and attitude control equipment) designed or modified for “missiles”.
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(These items are “subject to the ITAR”. See 22 CFR parts 120 through 130.)
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7A117 “Guidance sets” capable of achieving system accuracy of 3.33% or less of the range (e.g., a “CEP” of 10 km or less at a range of 300 km
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(These items are “subject to the ITAR”. See 22 CFR parts 120 through 130.)
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7A994 Other navigation direction finding equipment, airborne communication equipment
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The list of items controlled is contained in the ECCN heading.
Note 1) See also 7A005 and 7A105. (2) QRS11 Micromachined Angular Rate Sensors are “subject to the ITAR” (see 22 CFR parts 120 through 130), unless the QRS11-00100-100/101 is integrated into and included as an integral “component” of a commercial primary or standby instrument system of the type described in ECCN 7A994, or aircraft of the type described in ECCN 9A991 that incorporates such systems, or is exported solely for integration into such a system; or the QRS11-00050-443/569 is integrated into an automatic flight control system of the type described in ECCN 7A994, or aircraft of the type described in ECCN 9A991 that incorporates such systems, or are exported solely for integration into such a system. (See Commodity Jurisdiction requirements in 22 CFR Parts 121; Category VIII(e), Note(1).) In the latter case, such items are subject to the EAR.
Technology specific to the development and production of QRS11 sensors remains
“subject to the ITAR” (see 22 CFR parts
120 through 130).
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