Atlas6 is a best-in-class heavy-lift hybrid UAV with up to 10 hrs endurance, 50 kg payload, and 700 km range. Built for logistics, ISR, SAR, and counter-UAS missions, it delivers unmatched versatility, reliability, and mission-ready performance.
Spec Sheet
Configuration
Configuration
Multirotor-Hexacopter
Frame
Frame
Carbon fiber composite
Dimensions Un-Folded
Dimensions Un-Folded
260.6×113.7×138.4 cm (L×W×H)
Empty Weight
Empty Weight
45.6 kg
Weight with flight batteries
Weight with flight batteries
49 kg
Weight with 11L fuel load
Weight with 11L fuel load
57 kg
MTOW (fuel load + payload)
MTOW (fuel load + payload)
105 kg
Maximum payload
Maximum payload
56 kg
Max payload w/ 11L fuel load
Max payload w/ 11L fuel load
48 kg
Modular Payload system
Modular Payload system
Fuel Tanks Options
Fuel Tanks Options
6
Tank Sizes
Tank Sizes
11L, 22L, 33L, 44L, 55L
Ingress protection
Ingress protection
IP35
Connector Protection
Connector Protection
IP67
Rotors
Rotors
6
Rotor Diameter
Rotor Diameter
42
Blade Material
Blade Material
CFRP
Max Operating Temp
Max Operating Temp
-20° to +40° C
Sound w/ max payload @ 500m
Sound w/ max payload @ 500m
42 db10 Hours+ Max Endurance
50 Kilo Max Payload
- Hybrid Gas-Electric System
- Best-in-Class Payload Versatility
- Longest Flight Time in its Class
Flight Controller
Flight Controller
Cubepilot
Flight Computer
Flight Computer
PX4 based
w/Secondary backup
w/Secondary backup
fully Redundant Systems
Stabilization Modes
Stabilization Modes
Mission, stabilized, position hold etc.
Flight modes
Flight modes
Auto, loiter, altitude hold, RTH, land, guided (waypoints)
Onboard Processor
Onboard Processor
Jetson Nano
Operating System
Operating System
Linux
Mission Planning
Mission Planning
Mavlink
Max Airspeed
Max Airspeed
110 k/h (30.5 m/)
Cruise Airspeed
Cruise Airspeed
72 k/h (20 m/s)
Ascent Rate - continuous
Ascent Rate - continuous
3 m/s
Ascent Rate - peak
Ascent Rate - peak
10 m/s
Descent rate - continuous
Descent rate - continuous
2 m/s
Descent rate - peak
Descent rate - peak
5 m/s
Max Horiz. Speed (SL, no wind)
Max Horiz. Speed (SL, no wind)
21 m/s
Max Cross-wind
Max Cross-wind
15 m/s
Max Pitch Angle
Max Pitch Angle
35°
Max Altitude with 11L fuel tank/ no Payload
Max Altitude with 11L fuel tank/ no Payload
4300 m ASL
Max Altitude with 11L fuel tank/ max Payload
Max Altitude with 11L fuel tank/ max Payload
3000 m ASL
Operational Altitude
Operational Altitude
500 m ASL
Max Take Off altitude
Max Take Off altitude
3000 m ASL
Max flight time (ISA day, cruise speed, normal operating height) with 8 kg payload, 55L fuel load
Max flight time (ISA day, cruise speed, normal operating height) with 8 kg payload, 55L fuel load
9 hrs. 54 min (no reserve)
Max flight time (ISA day, cruise speed, normal operating height) with 50kg payload, 11L fuel load
Max flight time (ISA day, cruise speed, normal operating height) with 50kg payload, 11L fuel load
42 min (no reserve)
Max flight range (ISA day, cruise speed, normal operating height) with 8 kg payload, 55L Fuel load
Max flight range (ISA day, cruise speed, normal operating height) with 8 kg payload, 55L Fuel load
700 km
Max flight range (ISA day, cruise speed, normal operating height) with 50 kg payload, 11L fuel tank
Max flight range (ISA day, cruise speed, normal operating height) with 50 kg payload, 11L fuel tank
36 km
Thrust to weight ratio
Thrust to weight ratio
2:1 at max payload
Wind speed limits
Wind speed limits
15 m/s
Precip limits
Precip limits
waterproof in light precip
Engines
Engines
2
Displacement
Displacement
125 cc
Configuration
Configuration
2-Stroke Boxer
Max RPM
Max RPM
8300
Nominal RPM
Nominal RPM
7200
HP
HP
12
Cooling
Cooling
Liquid cooled
Fuel regulation
Fuel regulation
EFI
Fuel
Fuel
95 petrol + 2T oil mix (4%)
Fuel Consumption at TO, 50kg payload, 11L fuel
Fuel Consumption at TO, 50kg payload, 11L fuel
14 l/h
Fuel Consumption at cruise speed, 25kg payload, 10L fuel
Fuel Consumption at cruise speed, 25kg payload, 10L fuel
9 l/h
Fuel Consumption at hover, 10kg payload, 10L fuel
Fuel Consumption at hover, 10kg payload, 10L fuel
5 l/h
Generators
Generators
2
Peak Watts
Peak Watts
7000 watts
Peak amps
Peak amps
144 Amps
Nominal voltage
Nominal voltage
44.4-49.5V
Batteries
Batteries
4
Configuration
Configuration
Li Po 12s
Nominal capacity
Nominal capacity
5000 mAh
Continuous current
Continuous current
500A
Motors
Motors
6
Max watts per motor
Max watts per motor
5700
GCS open architecture
GCS open architecture
RF Telemetry/ Video
RF Telemetry/ Video
Silvus, DTC, Radinor, Creo, Persistent and other encrypted software defined
Data Link Redundancy
Data Link Redundancy
Starlink/ Satellite Link Integration
Starlink/ Satellite Link Integration
Mobile network - LTE modems
Mobile network - LTE modems
Fiber-optic
Fiber-optic
