Document ID: chunk:federal_register_of_legislation:F2017L00081:reg:25:p2
Version: federal_register_of_legislation:F2017L00081
Segment Type: reg
Provision Reference: reg 25 (pt 2/15)
Character Range: 161776–164745

consideration in determining range. The range for rocket systems will be determined independently of any external factors such as operational restrictions, limitations imposed by telemetry, data links, or other external constraints. For rocket systems, the range will be determined using the trajectory that maximises range, assuming International Civil Aviation Organization (ICAO) standard atmosphere with zero wind.
 (d) Technical data and defence services directly related to the defence articles described in paragraphs (a) to (c). (MT for technical data and defence services related to articles designated as such).
 (e) ‑ (w) [Reserved]
 (x) Commodities, software and technical data used in or with defence articles controlled in this category.
Note: Use of this paragraph is limited to exports of defence articles controlled in this category where the purchase documentation includes commodities, software or technical data.

Division 2—Missile Technology Control Regime

Missile Technology Control Regime
  The following items constitute all items on the Missile Technology Control Regime Annex which are covered by this list. To the extent an item mentioned in this Division is also mentioned elsewhere in Part 1, a reference appears in parentheses listing the category in which it appears.

Item 1—Category I
  Complete rocket systems (including ballistic missile systems, space launch vehicles, and sounding rockets (see Category IV(a) and (b)) and unmanned air vehicle systems (including cruise missile systems, see Category VIII (a), target drones and reconnaissance drones (see Category VIII (a)) capable of delivering at least a 500 kg payload to a range of at least 300 km.

Item 2—Category I
  Complete subsystems usable in the systems in Item 1 as follows:
 (a) individual rocket stages (see Category IV(h));
 (b) reentry vehicles (see Category IV(g)), and equipment designed or modified therefor, as follows, except as provided in Note 1 below for those designed for non‑weapon payloads;
 (1) heat shields and components thereof fabricated of ceramic or ablative materials (see Category IV(f));
 (2) heat sinks and components thereof fabricated of light‑weight, high heat capacity materials;
 (3) electronic equipment specially designed for reentry vehicles (see Category XI(a)(7));
 (c) solid or liquid propellant rocket engines, having a total impulse capacity of 1.1×10 N‑sec (2.5×10 lb‑sec) or greater (see Category IV, (h)).
 (d) "guidance sets" capable of achieving system accuracy of 3.33 percent or less of the range (for example, a CEP of 10 km or less at a range of 300 km), except as provided in Note 1 below for those designed for missiles with a range under 300 km or manned aircraft (see Category XII(d));
 (e) thrust vector control sub‑systems, except as provided in Note (1) below for those designed for rocket systems that do not exceed the range/payload capability of Item 1 (see Category IV);
 (f) warhead safing, arming, fuzing,