Division 01

Air Division

Fixed-wing, VTOL, and rotary platforms engineered for specific mission profiles. From tactical surveillance to agricultural operations and civil aviation training.

VTOL UAV
VL-03
Vertical-Launch Tactical Platform
Development

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.

Mission Profiles
  • Area surveillance and persistent ISR
  • Border and infrastructure monitoring
  • Search and rescue coordination
  • Civil mapping and photogrammetry
  • Disaster assessment and response support
Technical Specifications
Wingspan7.2 m
Length5.8 m
MTOW48 kg
Payload12 kg
Endurance6 h
Range280 km
Ceiling4,200 m
Cruise Speed95 km/h
PropulsionHybrid electric / EDF
Flight ControllerFC-3 (internal)
SensorEO/IR-9 (optional)
Fixed-Wing UAV
SR-12
Long-Endurance Surveillance System
Development

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.

Mission Profiles
  • Wide-area persistent surveillance
  • Coastal and maritime monitoring
  • Environmental data collection
  • Long-range photogrammetric mapping
  • Communications relay node
Technical Specifications
Wingspan12 m
Length7.4 m
MTOW120 kg
Payload24 kg
Endurance18 h
Range1,800 km
Ceiling6,000 m
Cruise Speed130 km/h
Data LinkCM-4A / 40 km
TakeoffRunway / catapult
Multi-Rotor UAV
MQ-4A
Agricultural Survey Platform
Prototype

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.

Mission Profiles
  • Precision agriculture mapping and NDVI analysis
  • Pesticide and fertilizer precision spraying
  • Infrastructure and power line inspection
  • Cadastral and topographic mapping
  • Construction site progress documentation
Technical Specifications
ConfigOctocopter (8 rotors)
Rotor Span1.8 m
MTOW18 kg
Endurance45 min
Payload6 kg
Max Speed65 km/h
IP RatingIP55
Battery SwapHot-swap system
Light Aircraft
LTA-1
Light Trainer Aircraft
Development

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.

Mission Profiles
  • Ab initio flight training (PPL / CPL)
  • Instrument rating training (IFR capable)
  • Flight school fleet standardization
  • Domestic aviation academy deployment
Technical Specifications
Config2-seat, low-wing monoplane
Wingspan9.8 m
Length7.1 m
MTOW750 kg
Vne185 kt (343 km/h)
Cruise130 kt
Range900 km
StructureCarbon fiber composite
CertificationEASA CS-VLA (target)
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