Passenger & Advanced Air Mobility

AIRMOBILITY M300

A low-altitude manned multi-rotor air mobility platform.

Dual seating configurationModular payload areaMulti-rotor design

Final specifications, options and availability are confirmed against the agreed configuration.

Technical highlights

Catalogue Specifications

Source: supplied catalogue reference page 15. Values are source claims; confirm the approved technical datasheet.
Payload300 kg
MTOW600 kg
Endurance45 min
Speed62 km/h
Operating Altitude500 m AGL
Wind ResistanceUp to 18 knots (40 km/h)
Maximum Distance40 km (turnaround distance)
Seating1 pilot + 1 passenger; payload configuration

Product overview

Key features

  • Dual seating configuration
  • Modular payload area
  • Multi-rotor design

Ask our team for the current technical datasheet and available configurations.

Applications

Explore the right use for your project.

01

Short-distance mobility

02

Supply requirements

03

Survey support

04

Rescue-support requirements

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