PEOPLE'S REPUBLIC OF CHINA (PRC) -- DRONES & UNMANNED AERIAL SYSTEMS
PEOPLE'S REPUBLIC OF CHINA (PRC) -- DRONES & UNMANNED AERIAL SYSTEMS
Last Updated: 2026-03-29 | Next Review Due: 2026-04-29
Classification: OPEN SOURCE / UNCLASSIFIED Compiled: 2026-03-28 Purpose: EOD identification, threat awareness, and UAS-delivered ordnance reference Maintainer: OSINT Research Cell
DISCLAIMER: This document is compiled exclusively from open-source, publicly available information. It is intended as a reference aid for EOD professionals to identify Chinese-origin UAS platforms and the munitions they carry. No classified or export-controlled information is included. Always defer to official technical publications for render-safe procedures. This document does NOT replace official EOD publications.
CROSS-REFERENCE: Loitering munitions CH-901, WS-43, and GJ-11 Sharp Sword are also documented in
ordnance_inventory.mdSection 10. Drone-delivered bombs (FT-series, LS-6) are in Section 6. This document provides expanded platform-level detail and the full UAS ecosystem.
TABLE OF CONTENTS
- Reconnaissance / ISR UAVs
- Armed / Strike UCAVs (MALE Class)
- Stealth and Advanced UCAVs
- Loitering Munitions
- Swarm-Capable Systems and Expendable UAVs
- Maritime UAS
- Small Tactical UAS
- Drone-Delivered Munitions Reference
- Export Customer Map
- Combat Employment Record
- Key Manufacturers
- Appendix A: EOD Hazard Summary for UAS
- Appendix B: UAS Visual Identification Guide
1. RECONNAISSANCE / ISR UAVs
1.1 BZK-005 -- Long-Endurance ISR UAV
| Parameter | Value |
|---|---|
| Chinese Designation | BZK-005 |
| NATO Reporting Name | None assigned |
| Type | Long-Endurance MALE ISR UAV |
| Manufacturer | BUAA (Beijing University of Aeronautics and Astronautics) / Harbin Aircraft Industry Group (AVIC) |
| First Flight | ~2006 |
| IOC (PLA) | ~2012 |
| Wingspan | 18 m (59 ft) |
| Length | 7.5 m (24.6 ft) |
| MTOW | 1,250 kg (2,756 lb) |
| Payload Capacity | 150 kg (330 lb) |
| Propulsion | Single piston engine (rear-mounted pusher) |
| Endurance | 40 hours |
| Service Ceiling | 8,000 m (26,250 ft) |
| Max Speed | 200 km/h (108 kt) |
| Cruise Speed | 130-150 km/h (70-81 kt) |
| Operational Radius | 2,400 km |
| Sensors | EO/IR turret, SAR (Synthetic Aperture Radar), SIGINT module (optional) |
| Guidance/Navigation | GPS/BeiDou + INS, SATCOM datalink |
| Armament | None (ISR only) |
| Source Rating | B-2 |
Operational Notes:
- Operated by PLAAF and PLA Navy (PLAN) aviation. Frequently observed in imagery from PLA airbases.
- Regularly patrols East China Sea and South China Sea. Tracked by JASDF intercepts since ~2013.
- Twin-boom pusher configuration, visually distinctive.
- Used for maritime surveillance, border patrol, and SIGINT collection.
EOD Relevance:
- Unarmed ISR platform. Primary hazard at crash site is fuel (AvGas or diesel), battery systems, and composite airframe dust.
- SIGINT payloads may contain sensitive electronic components -- intelligence value.
- Large airframe; debris field could be extensive.
Confidence: 1
1.2 BZK-007 -- Tactical ISR UAV
| Parameter | Value |
|---|---|
| Chinese Designation | BZK-007 |
| Type | Medium-Altitude Tactical ISR UAV |
| Manufacturer | BUAA / AVIC |
| Wingspan | ~8 m (26 ft) (estimated) |
| MTOW | ~300 kg (661 lb) |
| Payload Capacity | ~50 kg |
| Propulsion | Single piston engine (pusher) |
| Endurance | 12-16 hours |
| Service Ceiling | 5,000-7,000 m |
| Max Speed | ~200 km/h |
| Sensors | EO/IR turret |
| Guidance/Navigation | GPS/BeiDou + INS, LOS datalink |
| Armament | None confirmed |
| Source Rating | C-3 |
Operational Notes:
- Smaller companion system to BZK-005. Less commonly photographed or discussed in open sources.
- Likely used at brigade/division level for tactical ISR.
EOD Relevance:
- Unarmed. Fuel and battery hazards. Smaller debris footprint than BZK-005.
Confidence: 3
1.3 BZK-008 -- Advanced ISR UAV
| Parameter | Value |
|---|---|
| Chinese Designation | BZK-008 |
| Type | MALE-class ISR UAV |
| Manufacturer | BUAA / AVIC |
| Wingspan | ~18 m (estimated) |
| MTOW | ~1,500 kg (estimated) |
| Propulsion | Turboprop or heavy piston engine |
| Endurance | 24+ hours (estimated) |
| Service Ceiling | 8,000+ m |
| Sensors | EO/IR, SAR, ELINT |
| Source Rating | D-4 |
Operational Notes:
- Limited open-source information available. Believed to be an evolution of BZK-005 with improved sensors and endurance.
- Some sources suggest this designation may cover an upgraded BZK-005 variant rather than a wholly new platform.
EOD Relevance:
- Similar to BZK-005. Unarmed ISR platform.
Confidence: 4
1.4 WZ-7 Soaring Dragon (Xiang Long) -- High-Altitude ISR UAV
| Parameter | Value |
|---|---|
| Chinese Designation | WZ-7 (Wu Zhen-7, Unmanned Reconnaissance-7) |
| Alternative Names | Xiang Long (Soaring Dragon) |
| Type | High-Altitude Long-Endurance (HALE) ISR UAV |
| Manufacturer | Guizhou Aircraft Industry Corporation (GAIC) / AVIC |
| First Flight | 2011 |
| IOC (PLA) | ~2018-2020 |
| Wingspan | 25 m (82 ft) |
| Length | 14.3 m (47 ft) |
| Height | 5.4 m (17.7 ft) |
| MTOW | 7,500 kg (16,535 lb) |
| Payload Capacity | 650 kg (1,433 lb) |
| Propulsion | Single turbofan engine (likely WP-13 derivative) |
| Endurance | 10 hours (at altitude) |
| Service Ceiling | 18,000 m (59,000 ft) |
| Max Speed | 750 km/h (405 kt) |
| Cruise Speed | 600-650 km/h (324-351 kt) |
| Operational Radius | 7,000 km (estimated) |
| Sensors | Multi-sensor suite: EO/IR, SAR, ELINT/SIGINT, COMINT |
| Guidance/Navigation | GPS/BeiDou + INS, SATCOM datalink, pre-programmed autonomous flight |
| Armament | None (ISR only) |
| Source Rating | B-2 |
Key Feature -- Joined-Wing Configuration:
- Distinctive diamond/joined-wing planform. The rear wing connects to the tips of the forward wing, forming a box-wing structure.
- This configuration provides structural rigidity, high aspect ratio, and efficient high-altitude flight.
- Visually unmistakable -- no other operational UAV uses this planform.
Operational Notes:
- PLA's equivalent of the US RQ-4 Global Hawk in concept.
- Observed deployed to Yishuntun and Lingshui airfields. Confirmed in service with PLAAF.
- Designed for strategic ISR missions including maritime domain awareness over Western Pacific, South China Sea, and Indian Ocean.
- Satellite imagery has confirmed presence at bases near Taiwan and in Xinjiang.
EOD Relevance:
- Large jet-powered platform (7,500 kg). Crash site will involve significant jet fuel, large composite structures, and extensive debris field.
- High-altitude crash: debris may scatter over wide area.
- Composite airframe materials (carbon fiber, aramid) produce toxic particulates when burned.
- Jet fuel (kerosene-type) fire/explosion risk.
- High-value intelligence platform -- sensor payloads are priority exploitation items.
- NO weapons, but sensors may contain radioactive elements (certain IR detectors use HgCdTe or InSb cooled detectors).
Confidence: 1
1.5 WZ-8 -- Hypersonic / High-Speed Reconnaissance UAV
| Parameter | Value |
|---|---|
| Chinese Designation | WZ-8 (Wu Zhen-8, Unmanned Reconnaissance-8) |
| Alternative Names | None widely established |
| Type | High-Speed / Hypersonic Reconnaissance UAV |
| Manufacturer | BUAA / AVIC (believed) |
| Revealed | National Day Parade, October 1, 2019 |
| Wingspan | ~6.7 m (22 ft) |
| Length | ~11 m (36 ft) |
| Configuration | Delta wing with twin vertical stabilizers |
| Propulsion | Liquid-fueled rocket motor(s); air-launched from H-6 bomber |
| MTOW | ~3,000-5,000 kg (estimated) |
| Speed | Mach 3+ (some estimates Mach 5+) |
| Service Ceiling | 30,000+ m (98,000+ ft) (estimated) |
| Endurance | Minutes to tens of minutes (rocket-powered; non-loitering) |
| Operational Radius | ~800-2,000 km (dash and return profile) |
| Sensors | Likely multi-spectral imaging (EO, SAR), possibly ELINT |
| Launch Method | Air-launched from H-6N bomber (belly pylon) |
| Recovery | Conventional runway landing (retractable landing gear observed) |
| Armament | None (reconnaissance only) |
| Source Rating | C-2 |
Operational Notes:
- Displayed at 2019 parade on a transporter that indicates it is carried under the belly of the H-6N bomber.
- Designed for rapid, deep-penetration reconnaissance of heavily defended areas (carrier battle groups, Pacific island bases).
- Concept of operations likely similar to Cold War-era Lockheed D-21 drone.
- Liquid rocket propulsion makes this a high-speed dash vehicle, not a loitering platform.
- Some analysts assess it may serve a secondary strike role, but no weapons integration is confirmed.
EOD Relevance -- CRITICAL:
- LIQUID ROCKET PROPELLANT: Likely uses hypergolic or volatile liquid propellants (UDMH/NTO or similar). These are EXTREMELY toxic. Treat any crashed WZ-8 as a HAZMAT incident first.
- High-speed impact: If it crashes, the kinetic energy at Mach 3-5 will cause catastrophic destruction; debris will be small fragments spread over a wide area.
- Exotic materials: Likely uses titanium, ceramics, and ablative heat-shielding materials.
- Rocket motor: Even expended motors may contain residual propellant -- approach with extreme caution.
- H-6N pylons: If the mothership crashes, the WZ-8 may be found on its pylon -- treat as a combined aircraft/ordnance incident.
Confidence: 2
1.6 ASN-206 / ASN-207 -- Legacy Tactical ISR UAV
| Parameter | ASN-206 | ASN-207 |
|---|---|---|
| Chinese Designation | ASN-206 (Chang Hong-1) | ASN-207 |
| Type | Short-Range Tactical ISR UAV | Medium-Range Tactical ISR UAV |
| Manufacturer | Xi'an ASN Technology Group (Northwestern Polytechnical University) | |
| Wingspan | 6.0 m (19.7 ft) | 8.0 m (26.2 ft) |
| Length | 3.8 m (12.5 ft) | 5.0 m (16.4 ft) |
| MTOW | 222 kg (489 lb) | 480 kg (1,058 lb) |
| Payload | 50 kg (110 lb) | 80 kg (176 lb) |
| Propulsion | Piston engine (pusher) | Piston engine (pusher) |
| Endurance | 4-8 hours | 8-16 hours |
| Ceiling | 6,000 m (19,700 ft) | 6,000 m |
| Max Speed | 210 km/h | 210 km/h |
| Range | 150 km | 600 km |
| Sensors | EO daylight camera, IR camera | EO/IR, SAR |
| Launch | Rocket-assisted takeoff (RATO) | RATO or runway |
| Recovery | Parachute | Parachute or runway |
| Source Rating | B-2 | B-2 |
Operational Notes:
- Widely deployed PLA tactical UAV since 1990s. ASN-206 served as PLA's primary short-range ISR drone for over a decade.
- ASN-207 is the improved variant with longer endurance and enhanced sensors.
- Both use rocket-assisted takeoff from rail launchers and parachute recovery.
- Being progressively replaced by newer systems but likely still in PLA inventory in large numbers.
Export History:
- ASN-206 exported to Myanmar, Pakistan (reportedly), and possibly others.
EOD Relevance:
- Parachute-recovery system includes pyrotechnic devices for parachute deployment.
- RATO booster: solid-propellant rocket booster may be found at launch site or still attached if system malfunctions. Contains energetic material.
- Small enough to be transported easily. Could be encountered in various states of assembly.
- Fuel (AvGas/diesel) and battery hazards.
Confidence: 1
1.7 GJ-1 / Wing Loong I -- Armed ISR (Covered in Section 2)
See Section 2.1 for the armed Wing Loong I. Its ISR configuration is identical minus the weapons pylons.
2. ARMED / STRIKE UCAVs (MALE CLASS)
2.1 Wing Loong I / GJ-1 (Pterodactyl I) -- Armed MALE UCAV
| Parameter | Value |
|---|---|
| Chinese Military Designation | GJ-1 (Gong Ji-1, Attack-1) |
| Export Designation | Wing Loong I / Pterodactyl I / Yi Long |
| Type | Medium-Altitude Long-Endurance (MALE) Armed UAV |
| Manufacturer | Chengdu Aircraft Industry Group (CAIG) / AVIC |
| First Flight | 2007 |
| IOC (PLA) | ~2013 |
| Wingspan | 14.0 m (45.9 ft) |
| Length | 9.05 m (29.7 ft) |
| Height | 2.77 m (9.1 ft) |
| MTOW | 1,100 kg (2,425 lb) |
| Empty Weight | 750 kg (1,653 lb) |
| Payload Capacity | 200 kg (441 lb) total; ~100 kg weapons |
| Propulsion | Single Rotax 914 piston engine (115 hp), rear pusher prop |
| Endurance | 20 hours |
| Service Ceiling | 5,300 m (17,400 ft) |
| Max Speed | 280 km/h (151 kt) |
| Cruise Speed | 150-180 km/h (81-97 kt) |
| Loiter Speed | 120 km/h (65 kt) |
| Operational Radius | 4,000 km ferry; ~200 km operational (LOS datalink limited) |
| Hardpoints | 2 underwing pylons |
| Sensors | Nose-mounted EO/IR turret with laser designator/rangefinder |
| Weapons | BA-7 ATGMs (2x), AR-1 semi-active laser-guided missile, TL-2 laser-guided missile, FT-7/FT-9 guided bombs, 50 kg GP bombs |
| Guidance/Navigation | GPS/BeiDou + INS; LOS datalink (C-band); optional SATCOM |
| Source Rating | B-1 |
Comparable to: US MQ-1 Predator (similar performance class)
Export Customers (Confirmed):
| Country | Quantity | Year(s) | Notes |
|---|---|---|---|
| UAE | 5 | 2011 | First export customer |
| Saudi Arabia | 5-10 | 2014-2017 | RSAF operations in Yemen |
| Egypt | 10+ | 2016-2018 | Joint production agreement signed |
| Kazakhstan | 3 | 2016 | |
| Pakistan | ~10+ | 2016-2018 | Designated Burraq locally? Unconfirmed |
| Uzbekistan | ~3 | 2018 | |
| Nigeria | 2+ | 2019-2020 | Counter-Boko Haram operations |
| Indonesia | 4 | 2019 | ATAR variant designation locally |
| Serbia | 9 (reported contract) | 2020 | Controversial EU-border sale |
Combat Use:
- Libya (2019-present): Operated by UAE in support of LNA forces. Multiple losses documented. Wreckage recovered by GNA forces. At least 2-3 confirmed shootdowns.
- Yemen (2015-present): Saudi Arabia and UAE employed Wing Loong I for ISR and strikes against Houthi targets.
- Nigeria: Used against Boko Haram/ISWAP in the northeast.
EOD Relevance:
- If recovered crashed with weapons: BA-7 or AR-1 missiles may be live on pylons. Semi-active laser seekers present no RF hazard when unpowered.
- AvGas fuel (Rotax 914 uses MOGAS/AvGas).
- Small aircraft -- could be mistaken for civilian UAV wreckage.
- Composite construction: carbon fiber skin over aluminum/composite frame.
- EO/IR turret in nose is fragile but does not present explosive hazard.
- KEY IDENTIFIER: Distinctive long, narrow fuselage with V-tail, ventral sensor turret, and rear pusher prop.
Confidence: 1
2.2 Wing Loong II / GJ-2 -- Advanced Armed MALE UCAV
| Parameter | Value |
|---|---|
| Chinese Military Designation | GJ-2 (Gong Ji-2, Attack-2) |
| Export Designation | Wing Loong II / Pterodactyl II |
| Type | MALE Armed/ISR UAV |
| Manufacturer | Chengdu Aircraft Industry Group (CAIG) / AVIC |
| First Flight | February 27, 2017 |
| IOC (PLA) | ~2018 |
| Wingspan | 20.5 m (67.3 ft) |
| Length | 11.0 m (36.1 ft) |
| Height | 4.1 m (13.5 ft) |
| MTOW | 4,200 kg (9,259 lb) |
| Empty Weight | ~2,500 kg |
| Payload Capacity | 480 kg (1,058 lb) total; 400 kg weapons |
| Propulsion | Single turboprop engine (possibly WJ-9 or imported), ~700 hp, rear pusher |
| Fuel Capacity | ~1,000 kg |
| Endurance | 32 hours (ISR config); 20 hours (armed) |
| Service Ceiling | 9,000 m (29,500 ft) |
| Max Speed | 370 km/h (200 kt) |
| Cruise Speed | 200-250 km/h (108-135 kt) |
| Operational Radius | ~1,500 km (with SATCOM); 250 km (LOS datalink) |
| Hardpoints | 6 underwing pylons (3 per wing) |
| Sensors | Nose-mounted FLIR/EO/IR ball turret with laser designator, maritime search radar (optional), SAR, SIGINT pod (optional) |
| Weapons | BA-7 ATGM, AR-1/AR-2 SALH missile, Blue Arrow-7 (BA-7), FT-7/FT-9/FT-12 guided bombs, LS-6-50 mini PGM, YZ-212/YZ-102A GPS bombs, HJ-10AE ATGMs |
| Max Weapons Load | 12 weapons (e.g., 12x BA-7 or mixed load) |
| Guidance/Navigation | GPS/BeiDou + INS, Ku-band SATCOM datalink (BLOS), C-band LOS datalink |
| Ground Station | Containerized GCS; 1 pilot + 1 sensor operator |
| Source Rating | B-1 |
Comparable to: US MQ-9 Reaper (similar performance class)
Export Customers (Confirmed/Reported):
| Country | Quantity | Year(s) | Notes |
|---|---|---|---|
| UAE | 3-5 | 2018 | Operational in Libya |
| Saudi Arabia | 5+ | 2017-2019 | Complementing Wing Loong I |
| Egypt | 10+ | 2018-2020 | Possible local assembly line |
| Algeria | 3+ | 2019 | |
| Pakistan | 25+ (reported large order) | 2018-2022 | Major order; used in FATA/Balochistan |
| Nigeria | 3-5 | 2021 | Anti-insurgency ops |
| Morocco | 4 (reported) | 2021 | |
| Jordan | 12 (reported) | 2020 | |
| Libya (LNA) | ~3 | 2019 | Via UAE; lost in combat |
| Indonesia | 6 (reported) | 2022 | |
| Serbia | Included in Wing Loong I/II package | 2020 |
Combat Use:
- Libya (2019-2020): Extensively used by UAE-backed LNA forces. Operated from Al-Jufra and Al-Khadim airbases. Multiple confirmed strikes on GNA positions. At least 3 airframes lost (crash/shootdown). Wreckage documented extensively by conflict monitors (Bellingcat, Janes, IHS Markit).
- Ethiopia (2021-2022): Reportedly employed by Ethiopian government forces (ENDF) against Tigray People's Liberation Front (TPLF). Strikes on civilian areas documented by UN investigators. Drones reportedly operated from Harar Meda airbase.
- Yemen (2015-present): Saudi/UAE operations.
- Iraq (2015-2018): Unconfirmed reports of Chinese drone use; Iraq evaluated but likely purchased CH-4B instead.
- Myanmar (2022-present): Reported transfer to Myanmar military (Tatmadaw); unconfirmed but satellite imagery shows UAS shelters at Myanmar airbases.
EOD Relevance -- CRITICAL (Armed Platform):
- WEAPONS ON PYLONS: Crashed Wing Loong II may have 1-6 live weapons still attached. BA-7/AR-1/AR-2 missiles have semi-active laser homing seekers and blast-fragmentation warheads. FT-series bombs have GPS/INS fuzes.
- FUEL: Turboprop uses Jet-A/JP-8 type fuel. Up to 1,000 kg onboard.
- SIZE: 20.5 m wingspan -- this is a large aircraft. Crash debris field comparable to a light aircraft.
- SATCOM ANTENNA: Dorsal satellite communications dome (fragile but not explosive).
- COMPOSITE AIRFRAME: Carbon fiber, fiberglass, Kevlar -- toxic particulates when burned or fragmented.
- KEY IDENTIFIER: Distinguished from Wing Loong I by larger size, V-tail (similar but larger), 6 pylons vs 2, turboprop vs piston engine.
- WRECKAGE EXPLOITATION: Wing Loong II wreckage from Libya has been extensively documented. Fuselage serial numbers, Chinese-language markings, and AVIC logos have been photographed on recovered debris.
Confidence: 1
2.3 Wing Loong III -- Next-Generation MALE UCAV
| Parameter | Value |
|---|---|
| Export Designation | Wing Loong III |
| Type | Advanced MALE Armed/ISR UAV |
| Manufacturer | CAIG / AVIC |
| Revealed | Zhuhai Airshow 2024 (model/mockup shown earlier) |
| Wingspan | ~23 m (75.5 ft) (estimated) |
| Length | ~12 m (39.4 ft) |
| MTOW | ~5,500 kg (12,125 lb) (estimated) |
| Payload Capacity | ~1,000 kg |
| Propulsion | Turboprop, more powerful than WL-II |
| Endurance | 36+ hours (estimated) |
| Service Ceiling | 10,000+ m |
| Hardpoints | 6-8 (estimated) |
| Features | Improved SATCOM, AI-assisted targeting, enhanced EW suite, optional SIGINT |
| Source Rating | C-3 |
Operational Notes:
- Limited confirmed information. Displayed at defense expos as a next-generation evolution of the Wing Loong II.
- Likely incorporates lessons from combat use of Wing Loong I/II in Libya, Yemen, and Ethiopia.
- Expected to feature improved engine, longer endurance, heavier weapons load, and more autonomous operation.
EOD Relevance:
- Same hazard profile as Wing Loong II but larger and with potentially heavier weapons load.
Confidence: 3
2.4 CH-3 Rainbow -- Light Armed MALE UAV
| Parameter | Value |
|---|---|
| Designation | CH-3 (Cai Hong-3, Rainbow-3) |
| Type | Light MALE Armed/ISR UAV |
| Manufacturer | CASC (11th Academy / China Academy of Aerospace Aerodynamics, CAAA) |
| First Flight | ~2008 |
| Wingspan | 8.0 m (26.2 ft) |
| Length | 5.5 m (18.0 ft) |
| MTOW | 640 kg (1,411 lb) |
| Payload Capacity | 60-100 kg |
| Propulsion | Single piston engine, rear pusher |
| Endurance | 12 hours |
| Service Ceiling | 5,000-6,000 m |
| Max Speed | 235 km/h (127 kt) |
| Hardpoints | 2 underwing pylons |
| Sensors | EO/IR turret with laser designator |
| Weapons | AR-1 laser-guided missile (2x), FT-5 50 kg guided bomb |
| Guidance/Navigation | GPS/BeiDou + INS, LOS datalink |
| Source Rating | B-2 |
Export Customers:
| Country | Quantity | Notes |
|---|---|---|
| Pakistan | ~10 | Pakistan Army |
| Nigeria | 3+ | Anti-insurgency |
| Myanmar | ~2 (reported) | Tatmadaw |
| Turkmenistan | ~3 (reported) |
EOD Relevance:
- Small armed UAV. May carry 2x AR-1 missiles. Laser-guided warhead with shaped charge.
- Piston engine uses AvGas/MOGAS.
- Small enough to be transported in a large truck.
Confidence: 2
2.5 CH-4 Rainbow -- Primary Export Armed UCAV
| Parameter | CH-4A (ISR) | CH-4B (Armed) |
|---|---|---|
| Designation | CH-4A | CH-4B |
| Type | MALE ISR UAV | MALE Armed UAV |
| Manufacturer | CASC / CAAA (11th Academy) | |
| First Flight | ~2012 | ~2013 |
| Wingspan | 18.0 m (59 ft) | 18.0 m (59 ft) |
| Length | 8.5 m (27.9 ft) | 8.5 m (27.9 ft) |
| Height | 3.2 m | 3.2 m |
| MTOW | 1,330 kg (2,932 lb) | 1,330 kg (2,932 lb) |
| Payload Capacity | 115 kg sensors | 345 kg total (weapons + sensors) |
| Propulsion | Single piston engine (rear pusher) | Same |
| Endurance | 30+ hours | 14 hours (armed) |
| Service Ceiling | 8,000 m (26,250 ft) | 7,000 m |
| Max Speed | 235 km/h (127 kt) | 235 km/h |
| Cruise Speed | 150-180 km/h | 150-180 km/h |
| Hardpoints | None | 4 underwing pylons |
| Sensors | EO/IR ball turret with laser designator | Same |
| Weapons | None | AR-1 SALH missile, BA-7, FT-5 50 kg guided bomb, FT-7 25 kg guided bomb, HJ-10E ATGM |
| Guidance/Navigation | GPS/BeiDou + INS, LOS datalink | Same, optional SATCOM |
| Source Rating | B-1 | B-1 |
Comparable to: US MQ-1 Predator (performance) with some MQ-9 sensor capabilities
Export Customers (CH-4B is the best-selling Chinese armed drone):
| Country | Quantity | Year(s) | Notes |
|---|---|---|---|
| Iraq | 10+ | 2015-2017 | Largest confirmed operator. Used extensively against ISIS in Anbar, Mosul. Multiple strikes documented. |
| Saudi Arabia | 5-10 | 2017 | RSGF operations |
| Jordan | 6+ | 2016-2018 | |
| Egypt | 8-10 | 2017 | |
| Algeria | 4+ | 2017 | |
| UAE | 3 | 2016 | Reportedly less satisfied, shifted to Wing Loong II |
| Pakistan | Unknown (small quantity) | 2015+ | Evaluation/operational |
| Turkmenistan | 3 | 2018 | |
| Ethiopia | 4-6 (reported) | 2021 | Used in Tigray conflict |
| Myanmar | 2-3 (reported) | 2022 |
Combat Use:
- Iraq (2015-2018): The CH-4B was Iraq's primary armed drone during the anti-ISIS campaign. Numerous strike videos released by Iraqi Ministry of Defense. AR-1 missile strikes on vehicles and personnel documented. At least one CH-4B lost during operations. Iraqi operators reported mixed reliability and lower accuracy than advertised.
- Saudi Arabia / Yemen (2017+): Used against Houthi targets. Performance reportedly uneven; at least one crash attributed to engine failure.
- Jordan: Operational with Royal Jordanian Air Force for border security.
- Ethiopia (2021-2022): Reported use in Tigray conflict alongside Wing Loong II. Satellite imagery and social media OSINT confirm drone shelters at Harar Meda and Bahir Dar.
- Libya: Limited use; UAE preferred Wing Loong II.
EOD Relevance -- CRITICAL:
- MOST LIKELY CHINESE UCAV TO BE ENCOUNTERED. Most widely exported Chinese armed drone.
- WEAPONS: Up to 4 weapons on underwing pylons. AR-1 missiles are SALH (Semi-Active Laser Homing) with blast-fragmentation warheads. FT-5/FT-7 bombs have impact-detonation fuzes with GPS/INS.
- AR-1 MISSILE UXO: AR-1 has been fired in combat multiple times (Iraq, Yemen). Unexploded AR-1 missiles from CH-4B strikes have been documented.
- FUEL: AvGas/MOGAS, ~300 liters.
- KEY IDENTIFIER: Inverted V-tail (distinct from Wing Loong's V-tail). High-mounted straight wing. Ventral sensor turret. Resembles MQ-1 Predator but with inverted-V tail.
- MARKINGS: Export versions typically have customer country markings, but CASC logos and Chinese serial numbers may be visible on internal components.
Confidence: 1
2.6 CH-5 Rainbow -- Heavy Armed MALE UCAV
| Parameter | Value |
|---|---|
| Designation | CH-5 (Cai Hong-5, Rainbow-5) |
| Type | Heavy MALE Armed/ISR UAV |
| Manufacturer | CASC / CAAA |
| First Flight | August 2015 |
| Wingspan | 21.0 m (68.9 ft) |
| Length | 11.0 m (36.1 ft) |
| MTOW | 3,300 kg (7,275 lb) |
| Payload Capacity | 1,200 kg (2,646 lb) total; 1,000 kg weapons |
| Propulsion | Single heavy-fuel piston engine (330 hp), rear pusher |
| Endurance | 60 hours (ISR); 30-40 hours (armed) |
| Service Ceiling | 9,000 m (29,500 ft) |
| Max Speed | 300 km/h (162 kt) |
| Cruise Speed | 180-220 km/h |
| Operational Radius | ~2,000 km (SATCOM); 250 km (LOS) |
| Hardpoints | 6 underwing pylons |
| Sensors | EO/IR turret, SAR, maritime search radar |
| Weapons | AR-1/AR-2, BA-7, FT-7, FT-9, FT-12, LS-6-50, 50/100 kg GP bombs, cruise missile (concept), anti-ship missile (concept) |
| Max Weapon Load | Up to 16 weapons (e.g., 16x AR-1 or mixed) |
| Guidance/Navigation | GPS/BeiDou + INS, Ku-band SATCOM, C-band LOS datalink |
| Source Rating | B-2 |
Comparable to: US MQ-9 Reaper (closest comparison; CH-5 claims greater endurance but lower ceiling/speed)
Export Customers:
| Country | Quantity | Notes |
|---|---|---|
| Saudi Arabia | Unknown (under contract) | PSDI co-production agreement |
| Egypt | Under negotiation (reported) | |
| Pakistan | Under evaluation (reported) |
Operational Notes:
- Intended as China's heavy armed UCAV, carrying up to 16 precision munitions.
- 60-hour endurance claim would make it one of the longest-endurance armed UAVs in the world, but this has not been independently verified.
- Heavy-fuel piston engine reportedly experienced reliability issues during testing.
- Fewer confirmed exports than Wing Loong II or CH-4B.
EOD Relevance:
- Same category as Wing Loong II. Up to 6 pylons with multiple weapons types.
- Heaviest weapons load of any Chinese export drone -- up to 1,000 kg of ordnance.
- Large airframe with significant fuel load.
Confidence: 2
2.7 CH-6 Rainbow -- Next-Generation Armed UCAV
| Parameter | Value |
|---|---|
| Designation | CH-6 (Cai Hong-6, Rainbow-6) |
| Type | Advanced MALE Armed/ISR UAV |
| Manufacturer | CASC / CAAA |
| Revealed | Zhuhai Airshow 2022 (full-scale mockup) |
| Wingspan | ~20.5 m (67 ft) |
| Length | ~10 m |
| MTOW | ~3,500-4,000 kg (estimated) |
| Propulsion | Turboprop |
| Endurance | 20+ hours (estimated) |
| Service Ceiling | 9,000+ m |
| Hardpoints | 6 |
| Features | Improved sensors, AI-assisted target recognition, enhanced datalink, modular payload bays |
| Source Rating | C-3 |
Operational Notes:
- Positioned as the successor to CH-4/CH-5 with modern avionics and AI capabilities.
- Turboprop engine addresses the reliability issues experienced with CH-5's heavy piston engine.
- Not yet confirmed in production or export.
EOD Relevance:
- Expected to carry same weapons suite as CH-4/CH-5 family.
Confidence: 3
2.8 CH-7 Rainbow -- Stealth UCAV
| Parameter | Value |
|---|---|
| Designation | CH-7 (Cai Hong-7, Rainbow-7) |
| Type | Stealth UCAV (flying wing) |
| Manufacturer | CASC / CAAA |
| Revealed | Zhuhai Airshow 2018 (full-scale model) |
| Wingspan | 22.0 m (72.2 ft) |
| Length | 10.0 m (32.8 ft) |
| Height | 3.1 m (10.2 ft) |
| MTOW | 13,000 kg (28,660 lb) |
| Payload Capacity | 2,000+ kg (internal weapons bays) |
| Propulsion | Single turbofan engine |
| Speed | High subsonic (~Mach 0.75) |
| Service Ceiling | 13,000 m (42,650 ft) |
| Endurance | 15+ hours |
| Operational Radius | ~2,000 km (estimated) |
| Configuration | Tailless flying wing (stealth) |
| Weapons | Internal weapons bays for PGMs and air-to-ground missiles |
| Sensors | AESA radar (reported), EO/IR, SIGINT |
| Source Rating | C-3 |
Operational Notes:
- CASC's stealth UCAV competitor to AVIC's GJ-11 Sharp Sword.
- Marketed for export at defense shows. Notably, the CH-7 is positioned as an exportable stealth drone -- something neither the US nor other major producers offer.
- Flying wing planform similar to US X-47B, nEUROn, or Taranis.
- Development status unclear. May have flown in prototype form but not confirmed operational.
EOD Relevance:
- Internal weapons bays present a significant hazard at crash sites -- weapons may be trapped inside wreckage.
- Stealth coatings contain radar-absorbing materials (RAM) which may include toxic compounds (e.g., carbonyl iron, ferrite tiles, conductive polymers).
- Large turbofan-powered aircraft -- major crash site.
- Intelligence priority: If this is encountered, it would be a high-value intelligence find.
Confidence: 3
2.9 WJ-700 -- High-Speed Armed ISR UAV
| Parameter | Value |
|---|---|
| Designation | WJ-700 (Wu Jian-700, unmanned attack) |
| Type | High-Speed MALE Armed Reconnaissance UAV |
| Manufacturer | CASIC (3rd Academy) |
| First Flight | January 11, 2021 |
| Wingspan | 16.0 m (52.5 ft) |
| Length | 10.0 m (32.8 ft) |
| MTOW | 3,500 kg (7,716 lb) |
| Payload Capacity | 480 kg |
| Propulsion | Single turboprop engine (rear pusher) |
| Endurance | 20 hours |
| Service Ceiling | 10,000 m (32,800 ft) |
| Max Speed | 700 km/h (378 kt) -- significantly faster than WL-II or CH-4 |
| Hardpoints | 6 underwing pylons |
| Sensors | EO/IR turret, SAR, maritime patrol radar |
| Weapons | Anti-ship missiles (CM-502KG), AR-1/AR-2, FT-series guided bombs |
| Guidance/Navigation | GPS/BeiDou + INS, SATCOM |
| Source Rating | C-2 |
Key Differentiator:
- Speed. At 700 km/h, the WJ-700 is significantly faster than Wing Loong II (370 km/h) or CH-4 (235 km/h). This is a turboprop-powered UAV optimized for rapid response and anti-ship missions.
- Anti-ship capability. The WJ-700 is specifically marketed with the CM-502KG anti-ship missile, making it the first Chinese export drone purpose-designed for maritime strike.
Operational Notes:
- Manufactured by CASIC, making it a competitor to the AVIC (Wing Loong) and CASC (CH-series) families from a different state defense corporation.
- No confirmed exports as of early 2026.
- High speed and anti-ship missile capability suggest a focus on maritime scenarios (South China Sea, Indian Ocean).
EOD Relevance:
- Anti-ship missiles (CM-502KG) are a substantial hazard: 100+ kg warhead, radar/IR terminal seeker.
- Higher speed = higher kinetic energy at crash/impact.
- Turboprop engine with JP-8 type fuel.
Confidence: 2
3. STEALTH AND ADVANCED UCAVs
3.1 GJ-11 Sharp Sword (Li Jian) -- Stealth UCAV
NOTE: This system is also covered in
ordnance_inventory.mdSection 10.3. Expanded detail below.
| Parameter | Value |
|---|---|
| Chinese Designation | GJ-11 (Gong Ji-11, Attack-11) |
| Alternative Names | Li Jian (Sharp Sword) |
| Type | Stealth Unmanned Combat Aerial Vehicle (UCAV) |
| Manufacturer | Hongdu Aviation Industry Group / AVIC (Shenyang Aircraft Corporation also involved) |
| First Flight | November 21, 2013 |
| Parade Debut | National Day Parade, October 1, 2019 |
| IOC (PLA) | ~2019-2021 (estimated) |
| Wingspan | 14.0 m (45.9 ft) |
| Length | 10.0 m (32.8 ft) |
| Height | ~2.7 m (8.9 ft) |
| MTOW | ~10,000 kg (22,046 lb) (estimated) |
| Configuration | Flying wing (tailless, blended body-wing, cranked kite planform) |
| Propulsion | Single turbofan (likely WS-13 or non-afterburning WS-19 derivative), S-shaped inlet for radar shielding |
| Speed | High subsonic (~Mach 0.8) |
| Service Ceiling | 15,000 m (49,200 ft) (estimated) |
| Endurance | ~4-6 hours (estimated with combat load) |
| Operational Radius | ~1,200-2,000 km (estimated) |
| Weapons | Internal weapons bays; expected to carry PGMs (LS-6, FT-series), air-to-ground missiles, anti-radiation missiles, and possibly small anti-ship missiles |
| Sensors | Reported AESA radar, EO/IR targeting system |
| Stealth Features | Full radar-absorbent coatings, planform alignment, internal weapons carriage, S-shaped inlet |
| Guidance/Navigation | GPS/BeiDou + INS, SATCOM datalink, autonomous waypoint navigation, possible AI-assisted operations |
| Source Rating | B-2 |
Operational Notes:
- PLA's premier operational stealth UCAV. Likely assigned to PLAAF or PLAN aviation.
- Designed to operate in contested airspace where Wing Loong/CH-series drones cannot survive.
- Intended to work alongside manned fighters (J-20, J-16) as a "loyal wingman" in the manned-unmanned teaming (MUM-T) concept.
- No confirmed export customers. Unlikely to be exported in the near term.
- 2019 parade display confirmed at least initial operational capability.
- Satellite imagery suggests deployment to several PLAAF bases.
EOD Relevance -- CRITICAL:
- INTERNAL WEAPONS BAYS: Live ordnance may be trapped inside fuselage wreckage. Access may be difficult.
- STEALTH MATERIALS: RAM coatings and composite structures may contain hazardous materials. Approach with respiratory protection.
- JET FUEL: Large internal fuel load (estimated 3,000-4,000 kg JP-type fuel).
- SIZE: 14 m wingspan, ~10,000 kg -- this is a substantial aircraft. Crash site equivalent to a fighter jet.
- INTELLIGENCE VALUE: Extremely high. Any recovered GJ-11 wreckage should be treated as a top-priority intelligence find. Stealth coatings, sensor systems, and flight control computers are all high-value items.
- AUTONOMOUS SYSTEMS: May contain AI/autonomous flight hardware that continues to operate post-crash (radio emissions, data transmission attempts).
Confidence: 2
3.2 FH-97 -- Loyal Wingman Drone
| Parameter | Value |
|---|---|
| Designation | FH-97 (Fei Hong-97) |
| Type | Expendable / attritable loyal wingman UAV |
| Manufacturer | CASC / CAAA |
| Revealed | Zhuhai Airshow 2022 |
| Wingspan | ~10 m (estimated) |
| Length | ~9 m (estimated) |
| MTOW | ~3,000 kg (estimated) |
| Propulsion | Single turbofan engine, ventral intake |
| Speed | High subsonic |
| Service Ceiling | ~15,000 m |
| Endurance | ~2-4 hours (estimated) |
| Configuration | Stealthy aerodynamic shape with DSI inlet, V-tail |
| Weapons | Internal weapons bay, possible external pylons |
| Role | Air combat, EW, ISR, strike in support of manned fighters |
| Source Rating | C-3 |
Operational Notes:
- CASC's answer to the US Air Force's Collaborative Combat Aircraft (CCA) / XQ-58A Valkyrie concept.
- Designed to be relatively low-cost and attritable -- acceptable losses in combat.
- Operates in conjunction with J-20 or other manned fighters.
- Early development; not yet confirmed in PLA service.
EOD Relevance:
- Designed to be expendable, so encounters with crashed/disabled FH-97s may be more likely than with higher-value platforms.
- Turbofan engine, jet fuel, possible internal weapons.
- Stealth composite construction with RAM coatings.
Confidence: 3
3.3 Fei Hong (FH-95) / Dark Sword -- High-Speed Loyal Wingman Concepts
| Parameter | Value |
|---|---|
| Designations | FH-95 / "Dark Sword" (An Jian) |
| Type | High-speed / supersonic UCAV concepts |
| Manufacturer | AVIC / Shenyang Aircraft Corporation |
| Status | Concept / early development (Dark Sword shown as model ~2006-2018) |
| Configuration | Canard-delta configuration (Dark Sword) |
| Speed | Supersonic (Dark Sword concept) |
| Source Rating | D-4 |
Operational Notes:
- Dark Sword has been shown at various air shows as a model since 2006. A full-scale mockup was photographed in 2018.
- If developed, it would represent a supersonic UCAV capability that no other nation fields.
- Very limited confirmed information. May have been superseded by other programs (GJ-11, FH-97).
Confidence: 4
4. LOITERING MUNITIONS
NOTE: CH-901 and WS-43 are covered in detail in
ordnance_inventory.mdSection 10.1-10.2. This section provides additional loitering munition types.
4.1 CH-901 -- Man-Portable Loitering Munition
See ordnance_inventory.md Section 10.1 for full specifications.
Key recap for this document:
- 9 kg total, 3.5 kg warhead (shaped charge or fragmentation)
- 120 min loiter, 15 km range
- Tube-launched, electric propulsion
- Source Rating: B-1, Confidence 1
4.2 WS-43 -- Artillery-Launched Loitering Munition
See ordnance_inventory.md Section 10.2 for full specifications.
Key recap:
- 200 mm caliber, 20 kg warhead, 60 km range, 30 min loiter
- IR imaging terminal guidance
- Launched from rocket artillery pods
- Source Rating: C-2, Confidence 2
4.3 Blowfish A3 (Ziyan) -- Rotary-Wing Armed UAV / Loitering Munition
| Parameter | Value |
|---|---|
| Designation | Blowfish A3 |
| Type | Rotary-wing armed UAV / loitering weapon system |
| Manufacturer | Ziyan UAV (Shenzhen-based private company) |
| Configuration | Helicopter (single main rotor + tail rotor) |
| MTOW | 58 kg (128 lb) |
| Payload Capacity | 12 kg (26.5 lb) |
| Endurance | 2 hours |
| Max Speed | 130 km/h (70 kt) |
| Service Ceiling | 5,000 m |
| Range | 100 km |
| Weapons | 4x anti-personnel grenades (parachute-retarded), or 2x mortar rounds, or machine gun pod |
| Sensors | EO/IR camera, optional AI target recognition |
| Guidance/Navigation | GPS/BeiDou + INS, autonomous waypoint, AI target detection |
| Source Rating | C-2 |
Key Features:
- Autonomous weapons delivery. Ziyan has explicitly marketed the Blowfish A3 as capable of autonomous target engagement, including identifying and attacking targets without human input.
- Commercial-military crossover. Ziyan is a private Chinese drone company that also makes commercial UAVs. The Blowfish represents the blurring of military/commercial drone technology in China.
- Squad-level deployment. Small enough for infantry squad use.
Export Customers:
- Marketed at IDEX 2019 (Abu Dhabi). Specific export customers not publicly confirmed, but reportedly sold to unspecified Middle Eastern and Southeast Asian countries.
- Saudi Arabia: Reported interest/acquisition.
- UAE: Demonstrated at IDEX.
EOD Relevance:
- Helicopter configuration is unusual for a military UAV -- may be mistaken for a commercial drone.
- Grenades have parachute-retarded fuzes; if not detonated, they are live UXO.
- 12 kg payload could include various improvised or standardized submunitions.
- Lithium battery hazard. Electric motor.
- Autonomous operation means it may attempt to re-engage targets even after partial damage.
Confidence: 2
4.4 CASC FL-1 / FL-2 -- Fixed-Wing Loitering Munitions
| Parameter | FL-1 | FL-2 |
|---|---|---|
| Designation | FL-1 (Fei Lei-1) | FL-2 (Fei Lei-2) |
| Type | Loitering munition | Loitering munition (heavier) |
| Manufacturer | CASC / CAAA | CASC / CAAA |
| MTOW | ~5 kg | ~15 kg |
| Warhead | 1-2 kg (frag/shaped charge) | 5 kg (frag/shaped charge) |
| Endurance | 30-60 min | 60-90 min |
| Speed | 80-150 km/h | 80-150 km/h |
| Range | 10 km | 20-30 km |
| Launch | Hand-launched or catapult | Catapult or tube-launched |
| Guidance | EO seeker, GPS/BeiDou | EO seeker + IR, GPS/BeiDou |
| Source Rating | C-3 | C-3 |
EOD Relevance:
- Very small. FL-1 at 5 kg is hand-launched -- approaching commercial drone sizes.
- Live warheads in dud/crashed systems.
- Lithium battery fire hazard.
Confidence: 3
4.5 CASIC HW (Hai Ying / Sea Eagle) Series Loitering Munitions
| Parameter | Value |
|---|---|
| Designation | HW-1 through HW-series variants |
| Type | Family of loitering munitions (various sizes) |
| Manufacturer | CASIC |
| Range | 10-200 km (depending on variant) |
| MTOW | 5-50 kg (family range) |
| Warhead | 1-15 kg |
| Endurance | 30 min - 2 hours |
| Launch | Tube, vehicle, aircraft |
| Source Rating | C-3 |
Operational Notes:
- CASIC has displayed multiple loitering munition variants at defense expos.
- Some variants are designed for vehicle-launch (truck-mounted tubes, similar to Harop launcher concept).
- Specific export sales not confirmed in open sources.
Confidence: 3
4.6 NORINCO Battle Eagle (Zhan Ying) -- Ground-Launched Loitering Munition
| Parameter | Value |
|---|---|
| Designation | Battle Eagle / Zhan Ying |
| Type | Ground-launched loitering munition |
| Manufacturer | NORINCO |
| MTOW | ~10 kg |
| Warhead | 3 kg (fragmentation or shaped charge) |
| Endurance | ~60 min |
| Range | 15-20 km |
| Launch | Tube-launched (man-portable) |
| Guidance | EO seeker, GPS/BeiDou |
| Source Rating | C-3 |
EOD Relevance:
- Very similar profile to CH-901. Man-portable, tube-launched.
- May be encountered alongside NORINCO ground-force equipment exports.
Confidence: 3
5. SWARM-CAPABLE SYSTEMS AND EXPENDABLE UAVs
5.1 PLA Swarm Programs -- Overview
Source Rating: C-2
China has invested heavily in drone swarm technology and has demonstrated some of the world's largest coordinated UAV swarm flights:
Key Demonstrations:
- 2017: CETC (China Electronics Technology Group) demonstrated 119 fixed-wing drones in a coordinated swarm -- a world record at the time.
- 2018: CETC demonstrated 200+ drone swarm.
- 2020: Footage emerged of PLA ground forces launching swarms of small drones from vehicle-mounted tube launchers during exercises.
- 2022: CASIC demonstrated swarm-capable loitering munitions launched from truck-mounted pod launchers (48x tubes per launcher vehicle).
- 2023-2024: Multiple reports of PLA exercises incorporating drone swarm tactics at brigade level.
Known Swarm-Capable Platforms:
| Platform | Manufacturer | Launch Method | Type |
|---|---|---|---|
| CH-901 (in swarm config) | CASC | Multi-tube vehicle launcher (48 tubes) | Loitering munition swarm |
| CETC unnamed fixed-wing | CETC | Truck-launched or catapult | ISR/EW swarm |
| D21 series (expendable) | Various | Catapult, rocket | Expendable ISR/strike |
| Ziyan Swarm System | Ziyan | Multi-copter launcher | Rotary-wing swarm |
| CASC pod-launched swarm | CASC | Multi-tube pod on vehicle | Loitering munition |
Swarm Tactics (Assessed):
- Saturation attack: Overwhelm air defenses with large numbers of low-cost drones.
- ISR swarm: Distribute sensors across wide area for persistent surveillance.
- Communications relay: Self-organizing mesh network for battlefield comms.
- Decoy swarm: Saturate radar with false targets to cover manned aircraft ingress.
- Combined arms swarm: Mix of ISR, EW, and attack drones in a single coordinated swarm.
EOD Relevance -- CRITICAL:
- MASS UXO EVENTS. A swarm of 48+ loitering munitions from a single launcher could produce dozens of UXO items across a wide area if some fail to detonate.
- SMALL SIZE: Individual swarm drones may be as small as 1-5 kg. Extremely difficult to detect and catalog.
- BATTERY HAZARDS: Dozens of lithium batteries scattered across an area.
- MIXED WARHEADS: Swarm may include a mix of fragmentation and shaped-charge variants.
Confidence: 2
5.2 Expendable UAVs and Target Drones
| Platform | Manufacturer | Type | Notes |
|---|---|---|---|
| WZ-9 | AVIC | Target drone / decoy | Launched from aircraft; jet-powered |
| ASN-301 (Harpy clone) | BUAA/Xi'an | Anti-radiation loitering munition | Based on Israeli Harpy; attacks radar emitters. 20 kg warhead. |
| JWP-02 | Unknown | Target drone | |
| BQM-34 Chinese clone | Unknown | Target/decoy drone | Reverse-engineered from US BQM-34 Firebee |
ASN-301 -- Anti-Radiation Loitering Drone
| Parameter | Value |
|---|---|
| Designation | ASN-301 (believed to be CH designation for export) |
| Type | Anti-radiation loitering munition (DEAD/SEAD) |
| Origin | Based on Israeli IAI Harpy technology (licensed/reverse-engineered from 1994 sale) |
| Manufacturer | Xi'an ASN Technology / AVIC |
| Wingspan | 2.7 m (8.9 ft) |
| Length | 2.7 m (8.9 ft) |
| MTOW | 135 kg (298 lb) |
| Warhead | 20-30 kg blast-fragmentation |
| Propulsion | Small turbojet engine |
| Endurance | 4-6 hours |
| Speed | 185 km/h (100 kt) |
| Range | 200-300 km |
| Seeker | Wideband passive radar homing (anti-radiation) |
| Launch | Truck-mounted canister launcher (typically 18 per launcher vehicle) |
| Source Rating | B-2 |
EOD Relevance -- CRITICAL:
- ANTI-RADIATION MISSION: Passively homes on radar emissions. If it fails to find a target, it may crash with live warhead.
- TURBOJET ENGINE: Kerosene/jet fuel on board.
- 20-30 kg WARHEAD: Substantial blast-fragmentation warhead.
- CANISTER LAUNCH: Launch canisters contain propellant booster charges.
- MASS EMPLOYMENT: Deployed 18 per launcher vehicle. Multiple launcher vehicles in a battery = 50-100+ drones in a single DEAD attack.
- HARPY LINEAGE: If encountered, will closely resemble Israeli Harpy in configuration.
Confidence: 2
6. MARITIME UAS
6.1 Sea Eagle (Hai Ying) -- Maritime Patrol UAV Concept
| Parameter | Value |
|---|---|
| Designation | Various "Sea Eagle" maritime UAV concepts |
| Type | Maritime patrol / ASW UAV |
| Manufacturers | CASIC, CASC, various |
| Source Rating | D-3 |
Operational Notes:
- "Sea Eagle" or "Hai Ying" has been used as a marketing name for multiple maritime drone concepts shown at Chinese defense expos.
- China is actively developing ship-launched UAVs for PLAN destroyers and frigates.
- Specific operational systems include:
- Wing Loong II Maritime: Modified WL-II with maritime search radar and anti-ship capability.
- WJ-700: Specifically designed for maritime strike (see Section 2.9).
- TD-220: Tilt-rotor maritime UAV for shipboard deployment (VTOL capable).
6.2 TD-220 -- Tilt-Rotor Maritime UAV
| Parameter | Value |
|---|---|
| Designation | TD-220 |
| Type | Tilt-rotor VTOL UAV for maritime operations |
| Manufacturer | Tengdun Technology |
| MTOW | 220 kg (485 lb) |
| Payload | 50 kg (110 lb) |
| Endurance | 10 hours |
| Service Ceiling | 5,000 m |
| Range | 200 km |
| Configuration | Tilt-rotor (VTOL + fixed-wing cruise) |
| Sensors | EO/IR, maritime search radar, sonobuoy dispenser (ASW variant) |
| Source Rating | C-3 |
Operational Notes:
- Designed for deployment from PLAN warships (helicopter deck compatible).
- ASW variant can deploy sonobuoys and relay data to host ship.
- Tilt-rotor allows VTOL from confined ship decks with transition to efficient forward flight.
EOD Relevance:
- Ship-based recovery. May be encountered aboard captured/disabled PLAN vessels.
- Sonobuoy dispensers may contain expendable sonobuoys (battery-powered, some contain small explosive scuttling charges).
- Fuel and battery hazards.
Confidence: 3
6.3 PLAN Shipboard Helicopter UAVs
| Platform | Type | Ship Class | Notes |
|---|---|---|---|
| AVIC AR-500C | Unmanned helicopter | Type 054A frigates (tested) | 500 kg MTOW, coaxial rotor, EO/IR |
| S-100 (Chinese clone) | Unmanned helicopter | Various | Based on Schiebel S-100 Camcopter design |
| SVU-200 | Unmanned helicopter | Type 056 corvettes | Lightweight ISR |
EOD Relevance:
- Helicopter-type UAVs may carry fuel (AvGas/Jet-A) and have complex rotor mechanisms.
- If armed, weapons would be small (AR-1 class or grenades).
Confidence: 3
7. SMALL TACTICAL UAS
7.1 ASN-209 -- Brigade-Level Tactical UAV
| Parameter | Value |
|---|---|
| Designation | ASN-209 |
| Type | Tactical ISR UAV (brigade/division level) |
| Manufacturer | Xi'an ASN Technology |
| Wingspan | 7.5 m (24.6 ft) |
| Length | 4.3 m (14.1 ft) |
| MTOW | 320 kg (706 lb) |
| Payload | 50 kg (110 lb) |
| Propulsion | Piston engine, pusher |
| Endurance | 10 hours |
| Service Ceiling | 5,000 m |
| Max Speed | 200 km/h |
| Range | 200 km (LOS datalink) |
| Sensors | EO/IR turret |
| Launch | Rocket-assisted catapult (RATO) |
| Recovery | Parachute |
| Source Rating | B-2 |
Export Customers:
- Myanmar, reported. Used in anti-insurgency operations.
EOD Relevance:
- RATO booster: solid rocket motor at launch site.
- Parachute recovery system with pyrotechnic deployment charge.
- Unarmed ISR platform.
Confidence: 2
7.2 DJI Military-Modified Commercial Drones
| Parameter | Value |
|---|---|
| Manufacturer | DJI (Da-Jiang Innovations, Shenzhen) |
| Type | COTS commercial drones modified for military/paramilitary use |
| Models of Concern | Mavic 3, Matrice 300/350 RTK, Phantom 4 Pro, Inspire 2, Agras T-series |
| Source Rating | B-1 |
Context -- CRITICAL FOR EOD: DJI is the world's largest consumer/commercial drone manufacturer (~70-75% global market share). While DJI is not a military contractor, its drones have been extensively modified for military use worldwide:
Military Modifications Encountered:
| Modification | Description | Where Documented |
|---|---|---|
| Grenade/bomb drops | 3D-printed or machined release mechanisms carrying 40mm grenades, mortar rounds, thermite, VOG-17 grenades | Ukraine-Russia conflict, Myanmar, Iraq |
| ISR for artillery | Used for target acquisition and artillery correction | Ukraine, Syria, Myanmar, Libya |
| IED delivery | Modified to carry and release IEDs/submunitions | Iraq (ISIS), Syria, Myanmar |
| Chemical delivery | Concept for dispersal of agents (not confirmed in use) | Threat assessment |
| FPV kamikaze | Converted to one-way attack drones (less common for DJI; more common with purpose-built FPV) | Ukraine |
EOD Relevance -- EXTREMELY HIGH:
- DJI drones modified as weapons delivery platforms are among the most commonly encountered drone threats to EOD teams worldwide.
- Lithium polymer (LiPo) batteries: fire/thermal runaway.
- Modified drones may carry live grenades, mortar rounds, or IEDs with improvised fuzing.
- Small size (Mavic 3 weighs only 895 g without payload) makes them extremely difficult to detect.
- DJI's AeroScope system can detect and identify DJI drones, but modified firmware can disable this.
- Chinese government has implemented some export controls on DJI drones to conflict zones, but enforcement is limited.
Confidence: 1
7.3 Squad-Level Reconnaissance Micro UAVs
| Platform | Manufacturer | Type | MTOW | Endurance | Notes |
|---|---|---|---|---|---|
| HW-Mini | CASIC | Fixed-wing micro UAV | 2 kg | 90 min | Hand-launched, backpack-carried |
| Dove (Xin Ge) | Northwestern Polytechnical | Bird-shaped flapping wing | 0.2 kg | 30 min | Bio-mimetic; resembles a dove in flight |
| S-100 Mini | Various | Quad-rotor | 3-5 kg | 30 min | Commercial-derived, military-hardened |
| JH-7 (not the fighter) | CASC | Mini quad-rotor | 1.5 kg | 20 min | Individual soldier ISR |
"Dove" (Xin Ge) Program:
- Notable bio-mimetic drone program from Northwestern Polytechnical University.
- Flapping-wing drone designed to look and fly like a bird.
- Reported to have been tested by PLA for covert surveillance.
- At 200 grams, virtually undetectable.
- No weapons capability; purely ISR.
- Source Rating: C-3
Confidence: 3
8. DRONE-DELIVERED MUNITIONS REFERENCE
This section catalogs the air-to-ground weapons specifically integrated with Chinese UAS platforms.
8.1 AR-1 -- Semi-Active Laser Homing Missile
| Parameter | Value |
|---|---|
| Designation | AR-1 (export: Blue Arrow-1) |
| Type | Air-to-ground semi-active laser homing (SALH) missile |
| Manufacturer | CASC / CAAA |
| Length | 1.4 m (4.6 ft) |
| Diameter | 130 mm (5.1 in) |
| Weight | 45 kg (99 lb) |
| Warhead | 10 kg shaped charge + fragmentation sleeve |
| Warhead Effect | Penetrates 1,000 mm (1 m) RHA equivalent; lethal fragmentation radius ~15 m |
| Range | 2-8 km (launch from altitude) |
| Speed | Mach 1.1 (terminal) |
| Guidance | Semi-active laser homing (SAL); target must be illuminated by launching drone's laser designator |
| Fuze | Impact + slight delay |
| Launch Platforms | Wing Loong I, Wing Loong II, CH-3, CH-4B, CH-5 |
| Source Rating | B-1 |
EOD Relevance:
- MOST COMMON CHINESE DRONE-FIRED MISSILE. Multiple combat firings documented (Iraq, Libya, Yemen).
- Shaped-charge + fragmentation warhead. If unexploded, the shaped charge liner (copper or tantalum) is intact and warhead is armed.
- Impact fuze with delay -- duds are possible (fuze malfunction, insufficient impact angle, low-altitude skip).
- Semi-active laser seeker in nose is a glass dome over an optical detector -- fragile.
- Rocket motor is solid-propellant; residual propellant may be present in UXO.
- Small missile (45 kg, 1.4 m) -- could be mistaken for a commercial rocket or hobby missile.
Confidence: 1
8.2 AR-2 -- Lightweight SALH Missile
| Parameter | Value |
|---|---|
| Designation | AR-2 (export: Blue Arrow-2) |
| Type | Lightweight air-to-ground SALH missile |
| Manufacturer | CASC / CAAA |
| Length | 1.0 m (3.3 ft) |
| Diameter | ~100 mm |
| Weight | 25 kg (55 lb) |
| Warhead | 5-8 kg (shaped charge + frag) |
| Range | 2-8 km |
| Guidance | Semi-active laser homing |
| Launch Platforms | Wing Loong II, CH-4B, CH-5 |
| Source Rating | C-2 |
EOD Relevance:
- Smaller version of AR-1. Same hazard profile but lighter.
- Even easier to overlook as UXO due to small size.
Confidence: 2
8.3 BA-7 (Blue Arrow-7) -- Laser-Guided ATGM
| Parameter | Value |
|---|---|
| Designation | BA-7 / Blue Arrow-7 / Lan Jian-7 |
| Type | Air-launched anti-tank guided missile (ATGM) |
| Manufacturer | NORINCO |
| Length | 1.85 m (6.1 ft) |
| Diameter | 170 mm (6.7 in) |
| Weight | 47 kg (103 lb) |
| Warhead | Tandem shaped charge (penetrates 1,400 mm RHA behind ERA) |
| Range | 2-12 km (from altitude) |
| Speed | Mach 1.0 (terminal) |
| Guidance | Semi-active laser homing (SALH) |
| Fuze | Impact (base-detonation with graze function) |
| Launch Platforms | Wing Loong I/II, CH-4B, CH-5, Z-10 attack helicopter |
| Source Rating | B-2 |
EOD Relevance:
- TANDEM WARHEAD. Two shaped-charge warheads in series. The precursor charge defeats ERA; main charge penetrates base armor. Both must be treated as live in UXO.
- Larger and heavier than AR-1. More difficult to overlook.
- Base-detonation fuze with graze function means it can detonate at shallow impact angles.
- Copper or depleted-uranium shaped-charge liner (material depends on variant).
Confidence: 2
8.4 TL-2 -- Laser-Guided Missile
| Parameter | Value |
|---|---|
| Designation | TL-2 / Tian Lei-2 |
| Type | Lightweight air-to-ground laser-guided missile |
| Manufacturer | AVIC / Luoyang |
| Weight | ~20-30 kg (estimated) |
| Warhead | ~5 kg blast-fragmentation |
| Guidance | Semi-active laser homing |
| Range | 2-8 km |
| Launch Platforms | Wing Loong series, CH-series |
| Source Rating | C-3 |
EOD Relevance:
- Small laser-guided missile. Similar hazard to AR-2 class.
Confidence: 3
8.5 FT-Series Mini Precision Guided Munitions (PGMs)
NOTE: Full FT-series coverage is in
ordnance_inventory.mdSection 6. This subsection covers only the variants specifically sized for drone carriage.
| Variant | Weight | Guidance | Drone Platforms | Notes |
|---|---|---|---|---|
| FT-7 | 25 kg (55 lb) | GPS/BeiDou + INS | WL-II, CH-4B, CH-5 | Smallest FT bomb; micro-munition class |
| FT-6 | 50 kg (110 lb) | GPS/BeiDou + INS | WL-II, CH-4B, CH-5 | Small-diameter bomb |
| FT-5 | 100 kg (220 lb) | GPS/BeiDou + INS | WL-II, CH-5, WJ-700 | Standard drone PGM |
| FT-9 | 50 kg | GPS/BeiDou + INS + IIR terminal | WL-II, CH-5 | FT-6 with imaging infrared terminal seeker |
| FT-12 | 25 kg | GPS/BeiDou + INS + SAL | WL-II | FT-7 with semi-active laser terminal seeker |
EOD Relevance:
- GPS/INS guidance means these bombs have active electronics (GPS receiver, flight computer, actuators for guidance fins).
- Impact fuze with safe/arm mechanism. Duds may have partially armed fuzes.
- FT-9 and FT-12 have dual-mode guidance (GPS + terminal seeker) -- more complex electronics.
- SMALL SIZE WARNING: FT-7 at 25 kg (55 lb) is very small for a guided bomb. FT-12 is even lighter. These can be easily overlooked on a battlefield.
Confidence: 2
8.6 LS-6 Mini Variants (Drone-Compatible)
| Variant | Weight | Range | Notes |
|---|---|---|---|
| LS-6-50 | 50 kg | ~15 km glide | Smallest LS-6 variant; wing-kit guided bomb |
| LS-6-100 | 100 kg | ~25 km glide | Small-diameter bomb equivalent |
EOD Relevance:
- Pop-out wings may deploy on impact or during descent. Wings contain actuators.
- GPS/BeiDou + INS guidance. Same electronic hazards as FT-series.
- See
ordnance_inventory.mdSection 6 for full LS-6 family details.
Confidence: 2
8.7 CM-502KG -- Lightweight Anti-Ship Missile (UAS-Launched)
| Parameter | Value |
|---|---|
| Designation | CM-502KG |
| Type | Lightweight anti-ship / air-to-ground missile |
| Manufacturer | CASIC |
| Length | ~2.5 m |
| Weight | ~100 kg (total); warhead ~30 kg |
| Range | 25 km |
| Speed | Subsonic |
| Guidance | Active radar homing or IIR terminal + INS/GPS midcourse |
| Fuze | Impact + delay (anti-ship: penetration + delay) |
| Launch Platform | WJ-700, possibly Wing Loong II (heavy pylon) |
| Source Rating | C-2 |
EOD Relevance:
- ACTIVE RADAR SEEKER: Millimeter-wave radar in nose. Potential RF emission hazard if powered.
- Anti-ship penetration warhead with delay fuze -- designed to detonate inside a ship's hull.
- If dud, delay fuze may still be sensitive.
- Small anti-ship missile -- unusual UXO find if encountered on land.
Confidence: 2
8.8 HJ-10AE -- Anti-Tank Missile (Drone-Launched Variant)
| Parameter | Value |
|---|---|
| Designation | HJ-10AE (Hong Jian-10AE, Red Arrow-10 Air-launched Export) |
| Type | Air-launched ATGM |
| Manufacturer | NORINCO |
| Length | ~1.8 m |
| Weight | ~43 kg |
| Warhead | Tandem shaped charge (1,400 mm RHA penetration claimed) |
| Range | 2-10 km |
| Guidance | Millimeter-wave radar + IIR dual-mode seeker (fire-and-forget) |
| Launch Platforms | Wing Loong II (reported), Z-10 helicopter |
| Source Rating | C-2 |
EOD Relevance:
- FIRE-AND-FORGET: Does not need continuous laser illumination. More autonomous than AR-1/BA-7.
- DUAL-MODE SEEKER: MMW radar + IIR. Both seekers are active electronics -- potential RF hazard.
- TANDEM WARHEAD: Two shaped charges; both live in UXO scenario.
Confidence: 2
9. EXPORT CUSTOMER MAP
9.1 Comprehensive Chinese Military Drone Exports
| Country | Systems Acquired | Approximate Quantity | Year(s) | Confirmed Combat Use |
|---|---|---|---|---|
| MIDDLE EAST | ||||
| UAE | Wing Loong I, Wing Loong II | 8-10 | 2011-2018 | Libya, Yemen |
| Saudi Arabia | Wing Loong I, Wing Loong II, CH-4B, CH-5 (planned) | 15-25 | 2014-2019 | Yemen |
| Iraq | CH-4B | 10+ | 2015-2017 | Anti-ISIS campaign |
| Jordan | CH-4B, Wing Loong II (reported) | 6-18 | 2016-2020 | Border security |
| Egypt | Wing Loong I, Wing Loong II, CH-4B | 20-30 | 2016-2020 | Sinai operations (reported) |
| Algeria | CH-4B, Wing Loong II (reported) | 7+ | 2017-2019 | None confirmed |
| Morocco | Wing Loong II (reported) | 4 | 2021 | None confirmed |
| AFRICA | ||||
| Nigeria | Wing Loong I, Wing Loong II, CH-3 | 8-10 | 2019-2021 | Anti-Boko Haram/ISWAP |
| Ethiopia | Wing Loong II, CH-4B (reported) | 6-10 | 2021 | Tigray conflict |
| Libya (via UAE) | Wing Loong I, Wing Loong II | 5-8 | 2019 | Libyan civil war |
| Sudan | Unspecified Chinese drones (reported) | Unknown | 2020s | Civil conflict (reported) |
| Zambia | Wing Loong I (reported) | 2-3 | 2020 | None |
| SOUTH/CENTRAL ASIA | ||||
| Pakistan | Wing Loong I, Wing Loong II, CH-3, CH-4B, ASN-206 | 40-50+ | 2013-2022 | FATA/Balochistan ops |
| Kazakhstan | Wing Loong I | 3 | 2016 | None |
| Uzbekistan | Wing Loong I | 3 | 2018 | None |
| Turkmenistan | CH-3, CH-4B | 3-6 | 2018 | None |
| SOUTHEAST ASIA | ||||
| Myanmar | Wing Loong I (reported), CH-3 (reported), ASN-209 | 5-10 | 2017-2022 | Anti-insurgency (reported) |
| Indonesia | Wing Loong I, Wing Loong II (under contract) | 4-10 | 2019-2022 | None confirmed |
| EUROPE | ||||
| Serbia | Wing Loong I/II | 9 (reported) | 2020 | None |
Total Estimated Chinese Military UAS Exports: 150-250+ airframes across 20+ countries (as of early 2026).
Key Trends:
- Price advantage: Chinese armed drones cost $1-5 million each vs. $20-30 million for US MQ-9 Reaper. This makes them accessible to smaller militaries.
- No political strings: China does not impose end-use restrictions or human rights conditions on drone sales, unlike the US (prior to 2020 MTCR policy changes).
- Package deals: China often sells drones as part of larger military packages including ground stations, training, maintenance, and munitions.
- Licensed production: Egypt and Saudi Arabia have signed agreements for local assembly/production of Wing Loong variants.
Source Rating: B-2 (aggregated from SIPRI, IISS, and multiple defense publications) Confidence: 2
10. COMBAT EMPLOYMENT RECORD
10.1 Iraq (2015-2018) -- Anti-ISIS Campaign
| Detail | Information |
|---|---|
| Platform | CH-4B |
| Operator | Iraqi Armed Forces |
| Theater | Anbar Province, Mosul, Salahuddin, Diyala |
| Munitions Used | AR-1 SALH missile, FT-series guided bombs |
| Targets | ISIS VBIEDs, technicals, fighting positions, IED emplacers |
| Effectiveness | Mixed. Iraqi operators reported lower reliability and accuracy than advertised. Multiple strikes documented on video. |
| Losses | At least 1 CH-4B lost (crash, non-combat) |
| Source Rating | B-1 |
EOD Implications:
- AR-1 missile duds from Iraqi CH-4B strikes may be encountered in former ISIS-held areas.
- Iraqi strike footage shows AR-1 impacts on vehicles and structures -- UXO pattern is typically a single impact point with fragmentation spread.
10.2 Libya (2019-2020) -- Libyan Civil War
| Detail | Information |
|---|---|
| Platforms | Wing Loong I, Wing Loong II |
| Operator | UAE (supporting LNA/Haftar forces) |
| Operating Bases | Al-Jufra Air Base, Al-Khadim Air Base |
| Munitions Used | BA-7, AR-1, guided bombs |
| Targets | GNA military positions, convoys, air defense sites |
| Effectiveness | Significant. Wing Loong II conducted extensive strike operations. |
| Losses | At least 3-4 Wing Loong I/II lost (shootdown by GNA air defenses, crashes). Wreckage extensively documented. |
| Source Rating | B-1 |
EOD Implications:
- Wing Loong wreckage recovered by GNA forces has been widely photographed. AVIC markings, serial numbers, and Chinese-language technical labels documented.
- Unexploded ordnance from Wing Loong strikes reported in Tripoli area.
- GNA forces captured intact Wing Loong munitions (BA-7/AR-1) from downed drones.
- Wing Loong crash sites in Libya provide the best open-source reference for identifying Chinese UCAV wreckage.
10.3 Yemen (2015-Present) -- Saudi/UAE Operations
| Detail | Information |
|---|---|
| Platforms | Wing Loong I, Wing Loong II, CH-4B |
| Operators | Saudi Arabia, UAE |
| Munitions Used | AR-1, BA-7 |
| Effectiveness | Limited documentation. |
| Losses | At least 1 crash attributed to engine failure (Wing Loong I, Saudi). |
| Source Rating | C-2 |
10.4 Ethiopia (2021-2022) -- Tigray Conflict
| Detail | Information |
|---|---|
| Platforms | Wing Loong II, CH-4B (reported) |
| Operator | Ethiopian National Defense Force (ENDF) |
| Operating Base | Harar Meda Air Base (confirmed via satellite imagery) |
| Targets | TPLF military formations, convoys, reportedly civilian areas |
| Effectiveness | Reportedly significant tactical impact; multiple strikes on TPLF columns. |
| Losses | Unknown |
| Controversy | UN investigators documented strikes on civilian areas and internally displaced persons (IDP) camps. |
| Source Rating | C-2 |
10.5 Myanmar (2022-Present) -- Civil Conflict
| Detail | Information |
|---|---|
| Platforms | Unspecified Chinese drones (Wing Loong I, ASN-209 reported) |
| Operator | Tatmadaw (Myanmar military) |
| Targets | Ethnic armed organizations (EAOs), PDF (People's Defense Force) positions |
| Effectiveness | Limited documentation. |
| Source Rating | D-3 |
10.6 Nigeria (2019-Present) -- Counter-Insurgency
| Detail | Information |
|---|---|
| Platforms | Wing Loong I, Wing Loong II, CH-3 |
| Operator | Nigerian Armed Forces |
| Targets | Boko Haram, ISWAP positions in northeast Nigeria |
| Effectiveness | Reported as useful for ISR; strike effectiveness not well-documented. |
| Source Rating | C-2 |
11. KEY MANUFACTURERS
11.1 AVIC -- Aviation Industry Corporation of China (UAS Division)
| Detail | Information |
|---|---|
| Full Name | Aviation Industry Corporation of China, Ltd. |
| Type | State-owned defense conglomerate |
| Key UAS Subsidiary | Chengdu Aircraft Industry Group (CAIG) -- Wing Loong family |
| Other UAS Subsidiaries | Hongdu Aviation (GJ-11), Guizhou Aircraft (WZ-7), Shenyang Aircraft (Dark Sword concepts) |
| Headquarters | Beijing |
| Key Products | Wing Loong I/II/III, GJ-1/GJ-2, GJ-11, WZ-7, FH-95 |
| Export Brand | "Wing Loong" for UAS; CATIC (China National Aero-Technology Import & Export Corp) handles exports |
| Sanctioned? | AVIC and subsidiaries are on the US Entity List and subject to ITAR restrictions |
11.2 CASC -- China Aerospace Science and Technology Corporation (UAS Division)
| Detail | Information |
|---|---|
| Full Name | China Aerospace Science and Technology Corporation |
| Type | State-owned defense/space corporation |
| Key UAS Subsidiary | CAAA (China Academy of Aerospace Aerodynamics, 11th Academy) |
| Headquarters | Beijing |
| Key Products | CH-3, CH-4, CH-5, CH-6, CH-7, CH-901, FH-97 |
| Export Brand | "Rainbow" (Cai Hong) series |
| Sanctioned? | Yes; US Entity List |
11.3 CASIC -- China Aerospace Science and Industry Corporation (UAS Division)
| Detail | Information |
|---|---|
| Full Name | China Aerospace Science and Industry Corporation |
| Type | State-owned defense corporation |
| Key Products | WJ-700, WS-43, CM-502KG (drone-launched), HW-series loitering munitions |
| Headquarters | Beijing |
| Sanctioned? | Yes; US Entity List |
11.4 Xi'an ASN Technology Group
| Detail | Information |
|---|---|
| Affiliation | Spin-off from Northwestern Polytechnical University |
| Key Products | ASN-206, ASN-207, ASN-209, ASN-301 (Harpy-type) |
| Headquarters | Xi'an, Shaanxi Province |
| Note | Pioneer of Chinese military UAV development; many PLA legacy systems |
11.5 Ziyan UAV (Private Sector)
| Detail | Information |
|---|---|
| Full Name | Ziyan (Purple Swallow) UAV |
| Type | Private defense technology company |
| Key Products | Blowfish A3 armed helicopter UAV |
| Headquarters | Shenzhen, Guangdong Province |
| Note | Represents growing role of private Chinese defense companies |
11.6 DJI (Da-Jiang Innovations)
| Detail | Information |
|---|---|
| Type | Commercial drone manufacturer |
| Military Role | NONE officially; products widely modified for military use by third parties |
| Headquarters | Shenzhen, Guangdong Province |
| Market Share | ~70-75% of global consumer/commercial drone market |
| Sanctioned? | On US Entity List (December 2020). US DoD identified as "Chinese military company" |
| Note | DJI has stated it does not support military applications. However, its products are the most commonly encountered drones in conflict zones worldwide. |
APPENDIX A: EOD HAZARD SUMMARY FOR UAS
A.1 General UAS Hazard Categories
| Hazard Category | Description | Applicable Systems |
|---|---|---|
| LIVE ORDNANCE | Unexploded weapons on pylons or in internal bays | All armed UCAVs (WL-I/II, CH-4B, CH-5, GJ-11) |
| MISSILE UXO | Drone-fired missile that failed to detonate | AR-1, AR-2, BA-7, HJ-10AE |
| BOMB UXO | Drone-dropped bomb that failed to detonate | FT-5/6/7, LS-6-50/100 |
| LOITERING MUNITION | Entire drone is the weapon; warhead is integral | CH-901, WS-43, ASN-301, FL-1/2, Blowfish A3 |
| JET/AVGAS FUEL | Liquid fuel fire/explosion risk | All fuel-powered UAS |
| LITHIUM BATTERY | Thermal runaway, fire, toxic fumes | All electric UAS, all hybrid UAS, modified commercial drones |
| ROCKET MOTOR | Solid-propellant residue in RATO boosters, loitering munition motors | ASN-206/207/209, WS-43, ASN-301, tube-launched systems |
| LIQUID PROPELLANT | Toxic hypergolic propellants | WZ-8 (CRITICAL) |
| COMPOSITE DUST | Toxic carbon fiber, aramid, fiberglass particulates at crash/fire sites | All modern UAS |
| RAM/STEALTH COATINGS | Radar-absorbing material, possibly toxic compounds | GJ-11, CH-7, FH-97 |
| RF EMISSION | Active radar seekers, datalinks, or autonomous systems still transmitting | CM-502KG, HJ-10AE, any UAS with active comms |
| PYROTECHNICS | Parachute deployment charges, RATO igniters | ASN-206/207/209, parachute-recovery systems |
A.2 Approach Protocol for Chinese UAS Crash Sites
- ASSUME ARMED until confirmed otherwise. Even "ISR-only" platforms may carry weapons.
- ESTABLISH EXCLUSION ZONE:
- Small UAS (under 25 kg): 100 m minimum
- Medium UAS (25-1,500 kg): 300 m minimum
- Large UCAV (over 1,500 kg): 500 m minimum
- Any system with anti-ship missile: 1,000 m minimum
- CHECK FOR FUEL: Avgas, JP-8/Jet-A, or diesel. Vapor hazard.
- CHECK FOR BATTERIES: Lithium polymer/lithium-ion. Do not puncture, crush, or expose to heat.
- CHECK PYLONS/BAYS: Count weapons stations. Compare to known loadout. If fewer weapons than hardpoints, missing weapons may be live UXO elsewhere.
- RF HAZARD: Maintain electronic silence near active seeker-equipped missiles (CM-502KG, HJ-10AE). Turn off transmitters within 100 m.
- INTELLIGENCE VALUE: All Chinese military UAS are intelligence-priority items. Preserve markings, serial numbers, flight computers, sensor data cards.
- DOCUMENTATION: Photograph all Chinese-character markings. These may identify manufacturer, lot number, and production date.
A.3 Weapons-Platform Cross-Reference
| Weapon | Primary UAS Platform(s) | Warhead | Weight | Guidance |
|---|---|---|---|---|
| AR-1 | WL-I/II, CH-3/4B/5 | Shaped charge + frag (10 kg) | 45 kg | SALH |
| AR-2 | WL-II, CH-4B/5 | Shaped charge + frag (5-8 kg) | 25 kg | SALH |
| BA-7 | WL-I/II, CH-4B/5 | Tandem shaped charge | 47 kg | SALH |
| TL-2 | WL-series, CH-series | Blast-frag (5 kg) | 20-30 kg | SALH |
| HJ-10AE | WL-II, Z-10 | Tandem shaped charge | 43 kg | MMW + IIR |
| FT-5 | WL-II, CH-5 | HE blast (GP bomb) | 100 kg | GPS/INS |
| FT-6 | WL-II, CH-4B/5 | HE blast (GP bomb) | 50 kg | GPS/INS |
| FT-7 | WL-II, CH-4B/5 | HE blast (GP bomb) | 25 kg | GPS/INS |
| FT-9 | WL-II, CH-5 | HE blast | 50 kg | GPS/INS + IIR |
| FT-12 | WL-II | HE blast | 25 kg | GPS/INS + SAL |
| LS-6-50 | WL-II, CH-5 | HE blast | 50 kg | GPS/INS (glide) |
| CM-502KG | WJ-700 | HE penetration (30 kg) | 100 kg | Radar/IIR + INS |
| CH-901 (integral) | Man-portable, vehicle, swarm | Shaped charge / frag (3.5 kg) | 9 kg | EO + GPS |
APPENDIX B: UAS VISUAL IDENTIFICATION GUIDE
B.1 Quick Visual Identification Keys
| Platform | Key Visual Feature | Tail Config | Size Class | Propulsion Clue |
|---|---|---|---|---|
| Wing Loong I | Narrow fuselage, ventral turret | V-tail | Medium (14 m WS) | Rear pusher prop (piston) |
| Wing Loong II | Larger WL-I, 6 pylons, dorsal SATCOM dome | V-tail | Large (20.5 m WS) | Rear pusher prop (turboprop) |
| CH-4B | MQ-1-like, inverted V-tail | Inverted V-tail | Medium (18 m WS) | Rear pusher prop (piston) |
| CH-5 | Large, high wing, 6 pylons | Inverted V-tail | Large (21 m WS) | Rear pusher prop (heavy piston) |
| CH-7 | Flying wing, no tail | None (flying wing) | Large (22 m WS) | Jet intake (dorsal) |
| GJ-11 | Cranked-kite flying wing | None (flying wing) | Large (14 m WS) | Jet intake (S-shaped, dorsal) |
| WZ-7 | Joined/diamond wing (unique) | Joined wing | Very large (25 m WS) | Jet (turbofan) |
| WZ-8 | Sharp delta, twin verticals | Twin vertical stabs | Medium (6.7 m WS) | No visible prop/intake (rocket) |
| WJ-700 | Conventional layout, large engine | V-tail | Large (16 m WS) | Rear pusher turboprop |
| BZK-005 | Twin-boom, pusher | Twin boom | Large (18 m WS) | Rear pusher prop (piston) |
| ASN-206 | Small, high wing, pusher | Twin boom | Small (6 m WS) | Rear pusher prop |
| CH-901 | Tube-launched, small, cruciform | Cruciform fins | Very small (1.2 m WS) | Electric (no visible engine) |
| ASN-301 | Delta wing, turbojet | Delta | Small (2.7 m WS) | Small turbojet |
B.2 Distinguishing Chinese UAS from US/Israeli/Turkish Equivalents
| Chinese System | Often Confused With | Key Differences |
|---|---|---|
| Wing Loong I | MQ-1 Predator | WL-I has V-tail (Predator has inverted-V); WL-I ventral fin |
| Wing Loong II | MQ-9 Reaper | WL-II has V-tail (Reaper has inverted-V); WL-II dorsal SATCOM is smaller |
| CH-4B | MQ-1 Predator | CH-4 inverted-V tail matches Predator, but CH-4B is slightly larger and wing planform differs |
| CH-5 | MQ-9 Reaper | CH-5 has piston engine (Reaper is turboprop); CH-5 inverted-V tail |
| GJ-11 | X-47B, nEUROn | GJ-11 cranked-kite differs from X-47B's lambda wing; GJ-11 is smaller |
| WZ-7 | RQ-4 Global Hawk | WZ-7's joined wing is completely distinct from Global Hawk's conventional layout |
| ASN-301 | IAI Harpy | Nearly identical (derived from Harpy); Chinese markings may be only difference |
APPENDIX C: SOURCE NOTES AND BIBLIOGRAPHY
All entries in this document are compiled from open-source intelligence (OSINT). Key source categories:
A-Rated Sources (Official):
- US Department of Defense Annual Report to Congress: Military and Security Developments Involving the People's Republic of China
- Congressional Research Service reports on Chinese military modernization
B-Rated Sources (Established Defense Publications):
- IISS Military Balance (annual)
- SIPRI Arms Transfers Database
- Jane's Defence Weekly / IHS Markit
- CSIS (Center for Strategic and International Studies) reports
- Army Recognition (defense equipment database)
- Global Security
C-Rated Sources (Reputable News/Analysis):
- Defense News, USNI News, The War Zone, National Interest
- Bellingcat (OSINT investigations, particularly Libya drone wreckage analysis)
- Royal United Services Institute (RUSI) reports
- Carnegie Endowment drone proliferation studies
- Zhuhai Airshow official materials and defense expo reporting
D-Rated Sources (OSINT/Social Media):
- X/Twitter defense analysts (verified track records)
- Satellite imagery analysis (Planet Labs, Maxar via open analysis)
- Conflict monitor organizations
General Confidence Methodology:
- Systems displayed at Chinese defense expos with official specifications: B-2 minimum
- Systems confirmed in PLA service via multiple imagery sources: B-1
- Systems observed in combat (Libya, Iraq, Yemen): B-1 to C-1 depending on documentation quality
- Systems known only from single reports or limited imagery: C-3 or D-4
- Future/concept systems shown only as models: C-3 to D-4
END OF DOCUMENT
This document should be updated regularly as new open-source information becomes available. Chinese UAS proliferation is accelerating rapidly. Last review: 2026-03-28.
Cross-reference with: ordnance_inventory.md (parent document), sources.md