(a) Rockets, space launch vehicles (SLVs), missiles, bombs, torpedoes, depth charges, mines, and grenades as follows:
(1) rockets, SLVs and missiles capable of delivering at least a 500 kg payload to a range of at least 300 km (MT);
(2) rockets, SLVs and missiles capable of delivering less than a 500 kg payload to a range of at least 300 km (MT);
(3) man‑portable air defence systems (MANPADS);
(4) anti‑tank missiles and rockets;
(5) rockets, SLVs, and missiles not meeting the criteria of subparagraphs (1) to (4);
(6) bombs;
(7) torpedoes;
(8) depth charges;
(9) anti‑personnel, anti‑vehicle, or anti‑armour land mines (for example, area denial devices);
(10) anti‑helicopter mines;
(11) naval mines;
(l2) fragmentation and high explosive hand grenades.
Note 1: “Range” is the maximum distance that the specified rocket system is capable of travelling in the mode of stable flight as measured by the projection of its trajectory over the surface of the Earth. The maximum capability based on the design characteristics of the system, when fully loaded with fuel or propellant, will be taken into 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.
Note 2: “Payload” is the total mass that can be carried or delivered by the specified rocket, SLV, or missile that is not used to maintain flight.
Note 3: This paragraph does not control model and high power rockets and kits thereof made of paper, wood, fibreglass, or plastic containing no substantial metal parts and designed to be flown with hobby rocket motors that are certified for consumer use. Such rockets must not contain active controls (for example, RF, GPS).
Note 4: “Mine” means a munition placed under, on, or near the ground or other surface area and designed to be exploded by the presence, proximity, or contact of a person or vehicle.
(b) Launchers for rockets, SLVs and missiles, as follows:
(1) fixed launch sites and mobile launcher mechanisms for any system enumerated in paragraphs (a)(1) and (2) (MT);
(2) fixed launch sites and mobile launcher mechanisms for any system enumerated in paragraphs (a)(3) to (5) (for example, launch tables, TOW missile, MANPADS).
Note 1: For controls on non‑SLV launcher mechanisms for use on aircraft, see Category VIII(h).
Note 2: For controls on launcher mechanisms that are integrated onto a vessel or ground vehicle, see Categories VI and VII, respectively.
Note 3: This paragraph does not control parts and accessories (for example, igniters, launch stands) specially designed for consumer use with model and high power rockets and kits thereof made of paper, wood, fibreglass, or plastic containing no substantial metal parts and designed to be flown with hobby rocket motors that are certified for consumer use.
(c) Apparatus and devices specially designed for the handling, control, activation, monitoring, detection, projection, discharge, or detonation of the articles in paragraphs (a) and (b) (MT for those systems enumerated in paragraphs (a)(1) and (2), and (b)(1)).
Note 1: This paragraph includes specialised handling equipment (transporters, cranes, and lifts) specially designed to handle articles enumerated in paragraphs (a) and (b) for preparation and launch from fixed and mobile sites. The equipment in this paragraph also includes specially designed robots, robot controllers, and robot end‑effectors, and liquid propellant tanks specially designed for the storage or handling of the propellants controlled in Category V, or other liquid propellants used in the systems enumerated in paragraphs (a)(1), (2) or (5).
Note 2: Aircraft Missile Protection Systems (AMPS) are controlled in Category XI.
(d) Rocket, SLV and missile power plants, as follows:
(1) except as enumerated in subparagraph (2) or (3) of this paragraph, individual rocket stages for the articles enumerated in paragraph (a)(1), (2) or (5) (MT for those stages usable in systems enumerated in paragraphs (a)(1) and (2));
(2) solid propellant rocket motors, hybrid or gel rocket motors, or liquid propellant rocket engines having a total impulse capacity equal to or greater than 1.1 × 106N·s (MT);
(3) solid propellant rocket motors, hybrid or gel rocket motors, or liquid propellant rocket engines having a total impulse capacity equal to or greater than 8.41 × 105N·s, but less than 1.1 × 106N·s (MT);
(4) combined cycle, pulsejet, ramjet, or scramjet engines (MT);
(5) air‑breathing engines that operate above Mach 4 not enumerated in subparagraph (4);
(6) pressure gain combustion‑based propulsion systems not enumerated in subparagraphs (4) and (5);
(7) rocket, SLV, and missile engines and motors, not otherwise enumerated in:
(i) subparagraphs (1) to (6) of this category; or
(ii) Category XIX.
Note: This paragraph does not control model and high power rocket motors, containing no more than 5 pounds of propellant, that are certified for consumer use.
(e) ‑ (f) [Reserved]
(g) Non‑nuclear warheads for rockets, bombs and missiles (for example, explosive, kinetic, EMP, thermobaric, shape charge and fuel air explosive (FAE)).
(h) Systems, subsystems, parts, components, accessories, attachments or associated equipment, as follows:
(1) flight control and guidance systems (including guidance sets) specially designed for articles enumerated in paragraph (a) (MT for those articles enumerated in paragraphs (a)(1) and (2));
(2) seeker systems specially designed for articles enumerated in paragraph (a) (for example, radiofrequency, infrared) (MT for articles enumerated in paragraphs (a)(1) and (2));
(3) kinetic kill vehicles and specially designed parts and components therefor;
(4) missile or rocket thrust vector control systems (MT for those thrust vector control systems usable in articles enumerated in paragraph (a)(1));
(5) MANPADS grip stocks and specially designed parts and components therefor;
(6) rocket or missile nozzles and nozzle throats, and specially designed parts and components therefor (MT for those nozzles and nozzle throats usable in systems enumerated in paragraphs (a)(1) and (2));
(7) rocket or missile nose tips, nose fairings, or aerospikes, and specially designed parts and components therefor (MT for those articles enumerated in subparagraphs (a)(1) and (2));
(8) re‑entry vehicle or warhead heat shields (MT for those re‑entry vehicles and heat shields usable in systems enumerated in subparagraph (a)(1));
(9) missile and rocket safing, arming, fusing, and firing (SAFF) components (to include target detection and proximity sensing devices), and specially designed parts therefor (MT for those SAFF components usable in systems enumerated in paragraph (a)(1));
(10) self‑destruct systems specially designed for articles enumerated in paragraph (a) (MT for those articles enumerated in paragraphs (a)(1) and (2));
(11) separation mechanisms, staging mechanisms, and interstages useable for articles enumerated in paragraph (a), and specially designed parts and components therefor (MT for those separation mechanisms, staging mechanisms, and interstages usable in systems enumerated in subparagraph (a)(1));
(12) post‑boost vehicles (PBV) (MT);
(13) engine or motor mounts specially designed for articles enumerated in paragraphs (a) and (b) (MT for those articles enumerated in paragraphs (a)(1) and (2) and (b)(1));
(14) combustion chambers specially designed for articles enumerated in paragraphs (a) and (d) and specially designed parts and components therefor (MT for those articles enumerated in subparagraphs (a)(1) and (2), (b)(1) and (d)(1) to (5));
(15) injectors specially designed for articles controlled in this category (MT for those injectors specially designed which are usable in systems enumerated in subparagraph (a)(1));
(16) solid rocket motor or liquid engine igniters;
(17) re‑entry vehicles and specially designed parts and components therefor not elsewhere specified in this category (MT);
(18) specially designed parts and components for articles controlled in paragraph (g) not elsewhere specified in this category;
(19) penetration aids and specially designed parts and components therefor (for example, physical or electronic countermeasure suites, re‑entry vehicle replicas or decoys, or submunitions);
(20) rocket motor cases and specially designed parts and components therefor (for example, flanges, flange seals, end domes) (MT for those rocket motor cases usable in systems enumerated in subparagraphs (a)(1) and (2) and for specially designed parts and components for hybrid rocket motors enumerated in subparagraphs (d)(2) and (3));
(21) solid rocket motor liners and rocket motor insulation (MT for those solid rocket motor liners usable in systems enumerated in subparagraph (a)(1) or specially designed for systems enumerated in subparagraph (a)(2); and rocket motor insulation usable in systems enumerated in subparagraphs (a)(1) and (2));
(22) radomes, sensor windows, and antenna windows specially designed for articles enumerated in paragraph (a) (MT for those radomes usable in systems enumerated in subparagraph (a)(1) and for any radomes, sensor windows, or antenna windows manufactured as composite structures or laminates specially designed for use in the systems and components enumerated in:
(i) subparagraph (a)(1) or (2); or
(ii) subparagraph (d)(1); or
(iii) subparagraph (8), (9), (17) or (25) of this paragraph;
(23) rocket or missile payload fairings;
(24) rocket or missile launch canisters (MT for those rocket or missile launch canisters designed or modified for systems enumerated in subparagraphs (a)(1) and (2));
(25) fuses specially designed for articles enumerated in paragraph (a) (for example, proximity, contact, electronic, dispenser proximity, airburst, variable time delay, or multi‑option) (MT for those fuses usable in systems enumerated in subparagraph (a)(1));
(26) rocket or missile liquid propellant tanks (MT for those rocket or missile liquid propellant tanks usable in systems enumerated in subparagraph (a)(1));
(27) rocket or missile altimeters specially designed for use in articles enumerated in subparagraph (a)(1) (MT);
(28) pneumatic, hydraulic, mechanical, electro‑optical, or electromechanical flight control systems (including fly‑by‑wire systems) and attitude control equipment specially designed for use in the rockets or missiles enumerated in subparagraph (a)(1) (MT for these systems which have been designed or modified for those enumerated in subparagraph (a)(1));
(29) umbilical and interstage electrical connectors specially designed for use in the rockets or missiles enumerated in subparagraph (a)(1) or (2) (MT);
(30) any part, component, accessory, attachment, equipment, or system that (MT for those articles designated as such):
Note 1: Subparagraph (1)—a guidance set integrates the process of measuring and computing a vehicle's position and velocity, that is navigation, with that of computing and sending commands to the vehicle's flight control systems to correct the trajectory.
Note 2: Subparagraph (17)—this subparagraph does not control spacecraft. For controls on spacecraft, see Category XV.
Note 3: Subparagraph (29)—this subparagraph also includes electrical connectors installed between the systems specified in subparagraph (a)(1) or (2) and their payload.
(i) Technical data and defence services directly related to the defence articles enumerated in paragraphs (a) to (h), including classified technical data, and defence services using the classified technical data. Defence services include the furnishing of assistance (including training) to a foreign person in the integration of a satellite or spacecraft to a launch vehicle, including both planning and onsite support, regardless of the jurisdiction, ownership, or origin of the satellite or spacecraft, or whether technical data is used. It also includes the furnishing of assistance (including training) to a foreign person in the launch failure analysis of a launch vehicle, regardless of the jurisdiction, ownership, or origin of the launch vehicle, or whether technical data is used. (MT for technical data and defence services related to articles designated as such.)
(j)‑(w) [Reserved]
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.