Document ID: chunk:federal_register_of_legislation:F2017L00081:reg:25:p7
Version: federal_register_of_legislation:F2017L00081
Segment Type: reg
Provision Reference: reg 25 (pt 7/15)
Character Range: 175517–178658

by Item 1 (see Category XV(d)(4)).
 (d) electronic assemblies and components specifically designed for military use and operation at temperatures in excess of 125 degrees C (see Category XI(a)(7)).
 (e) design technology for protection of avionics and electrical subsystems against electromagnetic pulse (EMP) and electromagnetic interference (EMI) hazards from external sources, as follows, (see Category XI(b)):
 (1) design technology for shielding systems;
 (2) design technology for the configuration of hardened electrical circuits and subsystems;
 (3) determination of hardening criteria for the above.
Note 1: Item 11 equipment may be exported as part of a manned aircraft or satellite or in quantities appropriate for replacement parts for manned aircraft.
Note 2: Examples of equipment included in this item:
(a) Terrain contour mapping equipment; and
(b) Scene mapping and correlation (both digital and analog) equipment; and
(c) Doppler navigation radar equipment; and
(d) Passive interferometer equipment; and
(e) Imaging sensor equipment (both active and passive);
Note 3: In subitem (a), laser radar systems embody specialized transmission, scanning, receiving and signal processing techniques for utilization of lasers for echo ranging, direction finding and discrimination of targets by location, radial speed and body reflection characteristics.

Item 12—Category II
  Launch support equipment, facilities and software for the systems in Item 1, as follows:
 (a) apparatus and devices designed or modified for the handling, control, activation and launching of the systems in Item 1, (see Category IV(c));
 (b) vehicles designed or modified for the transport, handling, control, activation and launching of the systems in Item 1, (see Category VII(d));
 (c) telemetering and telecontrol equipment usable for unmanned air vehicles or rocket systems, (see Category XI(a));
 (d) precision tracking systems:
 (1) tracking systems which use a translb nv installed on the rocket system or unmanned air vehicle in conjunction with either surface or airborne references or navigation satellite systems to provide real‑time measurements of in‑flight position and velocity, (see Category XI(a));
 (2) range instrumentation radars including associated optical/infrared trackers and the specially designed software therefor with all of the following capabilities (see Category XI(a)(3)):
 (i) angular resolution better than 3 milli‑radians (0.5 mils);
 (ii) range of 30 km or greater with a range resolution better than 10 metres RMS;
 (iii) velocity resolution better than 3 metres per second.
 (e) Software which processes post‑flight, recorded data, enabling determination of vehicle position throughout its flight path (see Category IV(i)).

Item 13—Category II
  Analog computers, digital computers, or digital differential analyzers designed or modified for use in the systems in Item 1 (see Category XI (a)(6), having either of the following characteristics:
 (a) rated for continuous operation at temperature from below minus 45 degrees C to above plus 55 degrees C; or
 (b) designed as ruggedized or "radiation hardened".
Note: