Fixed-wing, VTOL, and rotary platforms engineered for specific mission profiles. From tactical surveillance to agricultural operations and civil aviation training.
The VL-03 is a medium-class VTOL UAV designed for ISR (intelligence, surveillance, and reconnaissance) and civil area monitoring. Its hybrid wing-body configuration allows vertical departure from unprepared sites, followed by efficient fixed-wing cruise flight for extended range and endurance coverage.
The airframe integrates twin electric ducted fans for vertical lift and a pusher propulsion system for cruise. Control surfaces are conventional with fly-by-wire actuation managed by the FC-3 flight controller. Payload bay accepts the EO/IR-9 gimbal system or other sensor packages up to 12 kg.
| Wingspan | 7.2 m |
| Length | 5.8 m |
| MTOW | 48 kg |
| Payload | 12 kg |
| Endurance | 6 h |
| Range | 280 km |
| Ceiling | 4,200 m |
| Cruise Speed | 95 km/h |
| Propulsion | Hybrid electric / EDF |
| Flight Controller | FC-3 (internal) |
| Sensor | EO/IR-9 (optional) |
The SR-12 is a high-aspect-ratio fixed-wing UAV optimized for persistent wide-area coverage missions. Designed from the outset for minimal crew operation, the system features semi-autonomous mission management with waypoint navigation, loiter patterns, and automatic return-to-home.
The modular payload bay supports multiple sensor packages: the EO/IR-9 imaging system, synthetic aperture radar, and multi-spectral cameras. Ground data link is handled by the CM-4A encrypted communications module with a 40 km air-to-ground range.
| Wingspan | 12 m |
| Length | 7.4 m |
| MTOW | 120 kg |
| Payload | 24 kg |
| Endurance | 18 h |
| Range | 1,800 km |
| Ceiling | 6,000 m |
| Cruise Speed | 130 km/h |
| Data Link | CM-4A / 40 km |
| Takeoff | Runway / catapult |
The MQ-4A is a heavy-lift octocopter designed for precision agriculture, infrastructure inspection, and cadastral mapping. Its modular arm design allows field replacement of damaged arms without tools. A hot-swap battery system enables near-continuous operation when multiple battery sets are available on-site.
IP55 rated enclosure protects all electronics in dusty and light-rain conditions. The aircraft supports both manual piloting via RC link and fully autonomous flight via pre-programmed mission plans. Compatible with standard orthomosaic mapping software via onboard geotagged imagery.
| Config | Octocopter (8 rotors) |
| Rotor Span | 1.8 m |
| MTOW | 18 kg |
| Endurance | 45 min |
| Payload | 6 kg |
| Max Speed | 65 km/h |
| IP Rating | IP55 |
| Battery Swap | Hot-swap system |
The LTA-1 is a two-seat piston-engine trainer aircraft designed for ab initio pilot training in domestic flight academies. The airframe uses carbon fiber composite construction for a favorable empty weight fraction, enabling a 750 kg MTOW with full fuel, instructor, and student aboard.
The cockpit features a glass avionics suite with dual EFIS displays, a conventional control column with dual throw for instructor override, and a full envelope protection envelope in the primary flight computer. Designed to meet EASA CS-VLA certification framework, enabling international market access.
| Config | 2-seat, low-wing monoplane |
| Wingspan | 9.8 m |
| Length | 7.1 m |
| MTOW | 750 kg |
| Vne | 185 kt (343 km/h) |
| Cruise | 130 kt |
| Range | 900 km |
| Structure | Carbon fiber composite |
| Certification | EASA CS-VLA (target) |