Our Aircraft
Our fixed-wing unmanned aerial vehicles: all with carbon fibre composite airframes, fully autonomous take-off, flight and landing, and real-time image processing for target detection.
Fixed Wing · Fighter UAV 2026
AVCI-3AVCI-3 Specifications
- Take-off Weight (MTOW)
- 6.5 kg
- Empty Weight
- 2.8 kg
- Wingspan
- 2 m
- Fuselage Length
- 1.1 m
- Endurance
- 30 min
- Cruise Speed
- 16.4 m/s
- Stall Speed
- 13 m/s
- Flight Range
- 5 km
- Communication Range
- > 5 km
- Flight Altitude
- 150 m
- Wing Airfoil
- E216
- Tail
- V-tail (ruddervator), inverted NACA 4412
- Airframe Material
- Carbon fibre composite
- Autopilot
- CubePilot Cube Orange+ · ArduPlane
- AI Computer
- NVIDIA Jetson Orin NX 8 GB
- Camera
- Allied Vision Alvium 1800 · 2464×2064 @ 30 FPS
- Target Detection
- RF-DETR · 96% accuracy
- Motor
- SunnySky X4120 V3 550KV · 15×7 propeller
- Battery
- Tattu 6S 22.2 V 20000 mAh Li-Po
- Communication
- 5 GHz Ubiquiti Rocket M5 · 2.4 GHz ELRS RC link
6.5 KG TAKE-OFF WEIGHT, 2.8 KG EMPTY WEIGHT
2 M WINGSPAN, 1.1 M FUSELAGE LENGTH
30 MIN ENDURANCE, 16.4 M/S CRUISE SPEED
ONE-PIECE CARBON FIBRE COMPOSITE FUSELAGE, MODULAR WINGS AND V-TAIL
REAL-TIME TARGET DETECTION AND AUTONOMOUS LOCK-ON WITH RF-DETR ON JETSON ORIN NX
AUTONOMOUS KAMIKAZE DIVE AND QR TARGET DETECTION
AIR-DEFENCE ZONE AVOIDANCE WITH POLAR A* ROUTE PLANNING
TELEMETRY AND VIDEO OVER A SINGLE 5 GHZ LINK, 5+ KM RANGE
CUBE ORANGE+ AUTOPILOT, FULLY AUTONOMOUS TAKE-OFF AND LANDING
Fixed Wing · IMechE UAS Challenge 2026
SEBATSEBAT Specifications
- Empty Weight
- 7 kg
- Payload Capacity
- 3 kg (liquid)
- Take-off Weight (MTOW)
- 10 kg
- Wingspan
- 3 m
- Length
- ≈ 1.8 m
- Average Speed
- 16–17 m/s
- Competition
- IMechE UAS Challenge 2026
7 KG EMPTY WEIGHT, 3 KG LIQUID PAYLOAD CAPACITY
3 M WINGSPAN, APPROX. 1.8 M LENGTH
16–17 M/S AVERAGE SPEED
DESIGNED FOR THE IMechE UAS CHALLENGE 2026: LIQUID PAYLOAD MISSION
Fixed Wing · IMechE UAS Challenge 2025
TUNATUNA Specifications
- Take-off Weight (MTOW)
- 10 kg
- Payload Capacity
- 4 kg
- Wingspan
- 2.7 m
- Length
- 1.6 m
- Wing Area
- 0.905 m²
- Endurance
- 20 min
- Cruise Speed
- 15.45 m/s
- Stall Speed
- 11.24 m/s
- Flight Range
- 2 km
- Flight Altitude
- 60 m
- Wing Airfoil
- Eppler 214
- Tail
- Conventional tail, NACA 0012
- Airframe Material
- Carbon fibre composite
- Autopilot
- CubePilot Cube Orange+ · ArduPilot
- Motor
- T-Motor AT5220-A 380KV · 19×10 carbon propeller
- Battery
- Profuse 6S 22.2 V 16000 mAh Li-Po
- Communication
- RFD 868x telemetry · 2.4 GHz RC link
- Mission System
- Autonomous payload release mechanism
10 KG TAKE-OFF WEIGHT AND 4 KG PAYLOAD CAPACITY
2.7 M WINGSPAN, 1.6 M LENGTH, 0.905 M² WING AREA
20 MIN ENDURANCE, 15.45 M/S CRUISE SPEED
AUTONOMOUS TAKE-OFF, WAYPOINT NAVIGATION, PAYLOAD DROP AND LANDING
3-LAYER CARBON FIBRE FUSELAGE, BALSA-MDF WINGS AND TAIL
TAILDRAGGER DESIGN FOR A 10×10 M TAKE-OFF AND 10×20 M LANDING AREA
CUBE ORANGE+ AUTOPILOT, GEO-FENCE AND FLIGHT TERMINATION SYSTEM (FTS)
RFD 868x TELEMETRY, 2 KM RANGE
Fixed Wing · Fighter UAV
PENÇE-02PENÇE-02 Specifications
- Take-off Weight
- 10.5 kg
- Payload Capacity
- 2 kg
- Flight Range
- 10 km
- Communication Range
- 10 km
- Endurance
- 35 min
- Wingspan
- 2.6 m
- Airframe Material
- Carbon fibre composite
- Flight Mode
- Fully autonomous flight and landing
- Mission System
- Real-time image processing and target detection
10.5 KG TAKE-OFF WEIGHT AND 2 KG PAYLOAD CAPACITY
10 KM FLIGHT RANGE
CARBON FIBRE COMPOSITE AIRFRAME
35 MIN ENDURANCE, FULLY AUTONOMOUS FLIGHT AND LANDING
REAL-TIME IMAGE PROCESSING AND TARGET DETECTION
10 KM COMMUNICATION RANGE
2.6 M WINGSPAN
Fixed Wing · Fighter UAV
PENÇE-01PENÇE-01 Specifications
- Take-off Weight
- 7 kg
- Payload Capacity
- 1.5 kg
- Flight Range
- 10 km
- Communication Range
- 10 km
- Endurance
- 30 min
- Wingspan
- 1.8 m
- Airframe Material
- Carbon fibre composite
- Flight Mode
- Fully autonomous flight and landing
- Mission System
- Real-time image processing, target detection, autonomous target tracking and dogfight
7 KG TAKE-OFF WEIGHT AND 1.5 KG PAYLOAD CAPACITY
10 KM FLIGHT RANGE
CARBON FIBRE COMPOSITE AIRFRAME
30 MIN ENDURANCE, FULLY AUTONOMOUS FLIGHT AND LANDING
REAL-TIME IMAGE PROCESSING AND TARGET DETECTION
10 KM COMMUNICATION RANGE
1.8 M WINGSPAN
AUTONOMOUS TARGET TRACKING AND DOGFIGHT
Fixed Wing · Autonomous Mission
ZD-02ZD-02 Specifications
- Take-off Weight
- 11.3 kg
- Payload Capacity
- 3.5 kg
- Flight Range
- 10 km
- Endurance
- 25 min
- Airframe Material
- Carbon fibre composite
- Flight Mode
- Fully autonomous flight and landing
- Mission System
- Real-time image processing and target detection
11.3 KG TAKE-OFF WEIGHT AND 3.5 KG PAYLOAD CAPACITY
10 KM FLIGHT RANGE
REAL-TIME IMAGE PROCESSING AND TARGET DETECTION
25 MIN ENDURANCE, FULLY AUTONOMOUS FLIGHT AND LANDING
CARBON FIBRE COMPOSITE AIRFRAME
Fixed Wing · Autonomous Mission
ZD-01ZD-01 Specifications
- Take-off Weight
- 9.4 kg
- Payload Capacity
- 2.2 kg
- Flight Range
- 10 km
- Endurance
- 20 min
- Airframe Material
- Carbon fibre composite
- Flight Mode
- Fully autonomous flight and landing
- Mission System
- Real-time image processing and target detection
9.4 KG TAKE-OFF WEIGHT AND 2.2 KG PAYLOAD CAPACITY
10 KM FLIGHT RANGE
REAL-TIME IMAGE PROCESSING AND TARGET DETECTION
20 MIN ENDURANCE, FULLY AUTONOMOUS FLIGHT AND LANDING
CARBON FIBRE COMPOSITE AIRFRAME
Fixed Wing · Autonomous Mission
HÜMAHÜMA Specifications
- Take-off Weight
- 8 kg
- Payload Capacity
- 1.8 kg
- Flight Range
- 10 km
- Endurance
- 15 min
- Airframe Material
- Carbon fibre composite
- Flight Mode
- Fully autonomous flight and landing
- Mission System
- Real-time image processing and target detection
8 KG TAKE-OFF WEIGHT AND 1.8 KG PAYLOAD CAPACITY
10 KM FLIGHT RANGE
CARBON FIBRE COMPOSITE AIRFRAME
15 MIN ENDURANCE, FULLY AUTONOMOUS FLIGHT AND LANDING
REAL-TIME IMAGE PROCESSING AND TARGET DETECTION