M165 VTOL
Adapt. Achieve. Ascend.
Engineered for heavy missions and unpredictable terrain, this platform brings vertical agility and long-range performance together.
ROTATION MODEL
Heavy-Lift Capability
ISO-Compatible Cargo Space
Hybrid Power System
Optimized Fuel Consumption
Long-Range Operations
Fully Autonomous capability
PLATFORM CAPABILITIES
Heavy-Lift Capability
ISO-Compatible Cargo Space
Hybrid Power System
Optimized Fuel Consumption
Long-Range Operations
Fully Autonomous capability
Technical parameters
The M165 VTOL is a large-scale, heavy-duty UAV purpose-built for demanding cargo and operational needs. With its hybrid propulsion system, it can lift heavy payloads vertically like a helicopter and cruise long distances efficiently like a fixed-wing aircraft. Its ISO-compatible cargo bay ensures compatibility with standardized shipping systems, making it ideal for industrial logistics, defence supply chains, and humanitarian aid missions.
Wingspan
4.5 meters
Length
3.4 meters
Height
1.1 meters
Empty Weight
110 Kg
Gross Weight
150 Kg
Operational parameters
The M165 VTOL combines heavy payload capacity with long operational range, making it a versatile workhorse for strategic missions. Its strong climb rate and ability to operate from highaltitude locations allow it to function effectively in mountainous or remote regions. Designed for efficiency, the hybrid system delivers reliable performance while keeping fuel costs low, even on extended missions.
Cruise Speed
28 m/s
Fuel Capacity
30 L
Range
300 km
Max Altitude
5,500 meters
Payload
30 kg
Payload Capabilities
With a 30 kg payload limit and a standardized cargo bay, the M165 VTOL offers unmatched versatility for large-scale UAV transport. It can carry heavy humanitarian aid packages, defence supplies, or sensitive industrial equipment while ensuring safe and stable delivery.
Max Payload Capacity
30 kg
Cargo Bay Compatibility
Small ISO standard package space
Payload Flexibility
Supports cargo, medical equipment, sensors, and surveillance gear
Payload Security
Reinforced bay design for stability and shock resistance during flight
