A1-CM Furia
Product descripton: A1-CM Furia by Athlon Avia
Developed and manufactured by LLC SPC Athlon Avia since 2014, the A1‑CM “Furia” UAS is a flying‑wing, composite UAV (fiberglass, carbon fiber, kevlar) designed for tactical reconnaissance and fire correction in modern combat environments. The system has passed full state trials and has been officially adopted by the Armed Forces of Ukraine, with extensive operational use since 2014.
“Furia” features an automatic control system with inertial and satellite navigation, encrypted command and telemetry links with backup channels, and radio‑silence flight capability. It supports day and night payloads, including thermal imaging, enabling continuous ISR across varied conditions. Long flight endurance and extended command‑line range allow missions at tactical depth, while autonomous modes ensure return and mission continuity even without satellite navigation.
A standard system includes three UAVs, multiple day and night payloads, and a comprehensive spare‑parts set, ensuring high combat readiness and rapid field recovery. The GCS‑3 ground control station supports one or two operators and provides robust, mobile mission control with Linux‑based software, high‑brightness displays, hot‑swappable power, onboard charging, and full data handling—making the A1‑CM “Furia” a reliable, maintainable, and continuously upgraded ISR solution.
Technical specifications
Technical Characteristics
| Parameter | Specification |
|---|---|
| Type | Flying wing |
| Materials | Fiberglass, carbon fiber, Kevlar |
| Wingspan | 2000 mm |
| Length | 900 mm |
| Power Unit | Electric motor |
| Power Supply | Li‑ion batteries, 42 000 mAh |
| Takeoff Weight | 5.5 kg |
| Cruise Speed | 65 km/h |
| Maximum Range | 70 km |
| Route Length | Up to 200 km |
| Flight Time | Up to 4 hours |
| Wind Resistance | Up to 15 m/s |
| Launch Method | Elastic or mechanical catapult |
| Landing Method | Parachute or aircraft‑type landing |
| Flight Modes | Semi‑automatic guided, autonomous, camera‑guided |
Tactical Characteristics
| Capability | Description |
|---|---|
| Crew | 1–2 operators (depending on mission complexity) |
| Deployment Time | 15 minutes from stowed position |
| Takeoff & Landing | Fully automatic |
| Mission Flexibility | Route change possible during flight |
| Radio Silence Mode | Supported |
| GNSS Support | GPS, GLONASS, Galileo, BeiDou, QZSS, SBAS |
| GNSS‑Free Navigation | Autonomous optical flow navigation |
| Autonomous Return | Return‑to‑home without satellite navigation |
| Data Security | AES‑256 encrypted command line, redundant digital link |
| Targeting | Automatic target acquisition and tracking (static & moving) |
| Camera‑Guided Flight | Supported |
| Ground Control Station | Rotary antenna system with stepper motor |
| Mobile Operations | Mission execution while in motion |
| Software | Enhanced Linux‑based system |
| Integration | Compatible with artillery fire control systems |