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M-40 Vertical Takeoff And Landing Composite Wing Unmanned Aerial Vehicle

M-32 Vertical Takeoff And Landing Composite Wing Unmanned Aerial Vehicle

The M-32 Vertical Takeoff and Landing (VTOL) Composite Wing Unmanned Aerial Vehicle integrates the best of VTOL agility and fixed-wing efficiency, enabling runway-independent takeoff/landing in constrained or off-grid locations while delivering extended endurance for long-range missions. Built with premium lightweight composite materials, its rugged structure balances durability with enhanced payload capacity, supporting versatile equipment like high-res RGB cameras, thermal imagers, or LiDAR systems. Equipped with advanced autonomous flight controls, precise GPS navigation, and real-time data transmission, the M-32 excels in demanding professional scenarios—including large-area topographic mapping, industrial facility inspection, precision agriculture, and emergency response—offering reliable performance, extended operational range, and hassle-free deployment for industrial, commercial, and public sector users.

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Description

Parameter Details

  • Aircraft Type: Vertical Take-Off and Landing Composite Wing UAV
  • Empty Weight: <6kg
  • Aircraft Material: Autoclave-molded all-composite material
  • Take-off and Landing Method: Vertical Take-Off and Landing
  • Maximum Take-off Weight: 30kg
  • Payload: <10kg
  • Power System: V605KV210 + AT7215KV220
  • Battery: Custom 12S Battery
  • Flight Speed: 80-120km/h
  • Cruising Speed: 85-95km/h
  • Wind Resistance: Headwind Level 6
  • Flight Endurance: >260min (with 2.5kg counterweight)

Dimensions

  • Wingspan: 3.6m
  • Length: 1.82m (1.89m with pitot tube)
  • Ground clearance: >160mm
  • Fuselage: Carbon fiber composite with PVC foam core
  • Wings: Kevlar composite with PVC foam core
  • Vertical takeoff and landing boom: 3K carbon fiber

Flight Data

  • Takeoff Weight: 26 kg, Payload: 2.5 kg
  • Cruise Speed: 90 km/h, Cruise Time > 200 minutes, Range 366 km; Data tested at an altitude of 10 meters, 150 meters, and wind speeds of 3.4-7.0 m/s.
  • Takeoff Weight: 26.5 kg, Payload: 5 kg
  • Cruise Speed: 90 km/h, Cruise Time > 200 minutes, Range 283 km; Data tested at an altitude of 10 meters, 150 meters, and wind speeds of 3.4-7.0 m/s.
  • Takeoff Weight: 32 kg, Payload: 10 kg
  • Cruise Speed: 90 km/h, Cruise Time > 120 minutes, Range 196 km; Data tested at an altitude of 10 meters, 150 meters, and wind speeds of 3.4-7.0 m/s.
  • Packaging Dimensions: 1870*520*560 mm; 0.55 m³ (≤ 65 kg)

M-32 Vertical Takeoff And Landing Composite Wing Unmanned Aerial Vehicle

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