— f. III.r · sex-rotor, ad onus —

Vitruvius.

A six-rotor workhorse for inspection, cinematography, and remote-area logistics. Bamboo-lattice frame around a walnut hub — strong where it must be, light where it should be.

Class
Hexrotor · heavy lift
Frame
Bamboo lattice, walnut hub
Lift
5 kg sustained
Status
In design — Q3 flight testing
D · oculus, 3-axes Vitruvius — sex-rotor, ad onus view A: superius · scala 1:5 diametrum · 720mm brachium · 220mm f. III.r — bambusa, walnut, bio-resin

A quadrotor that loses a motor is a stone. A hexrotor that loses a motor is still a flying machine — degraded, but flying. For the missions Vitruvius is designed for — inspecting wind turbines, carrying payloads over forest, working in places where a controlled descent is not always available — that distinction is the whole point.

Six rotors also let us run each motor at lower load, which means smaller propellers, slower tip speeds, and a far quieter machine than a comparable quadcopter at the same lift.

The frame is a hexagonal lattice of bamboo splints woven around a central walnut hub. Vitruvian geometry is not decoration; it is how the structure works. Each of the six arms is supported by two neighbouring arms via tension members, distributing rotor loads across the whole frame rather than concentrating them at the hub.

The walnut hub is turned from reclaimed stock, drilled and pinned rather than glued. Every electronic component sits inside it, and every component is accessible by removing two pins.

Redundancy by design

Vitruvius runs two flight controllers in parallel — one primary, one dormant — with automatic crossover on fault. The IMU is triple-redundant. The power distribution is split: any three motors can fail and the airframe will continue to fly to a controlled landing.

Airframe

Frame
Bamboo lattice, walnut hub
Construction
Woven splints, bio-resin saturated
Joint detail
Mortise-and-tenon, brass pinning
Dry weight
2.4 kg
Diameter
720 mm motor-to-motor
Height
320 mm with gimbal

Propulsion

Motors
6 × 460 KV brushless
Propellers
17" composite
Battery
6S 22000 mAh, hot-swap
Lift
5 kg sustained · 8 kg burst
Endurance
32 minutes at 3 kg payload
Range
14 km telemetry-linked

Avionics

Flight controller
Dual-redundant, voting failover
GPS
RTK + dead-reckoning fallback
IMU
Triple-redundant
Comms
Mesh-capable LoRa + 5 GHz
Firmware
Open · audited · upgradable

Payload & gimbal

Payload bay
3 kg quick-release
Gimbal
3-axis stabilised, ± 0.01°
Standard sensor
Full-frame mirrorless interface
Power
12V / 24V regulated to bay
Mounts
Documented standard, third-party welcome
01

Hub

Black walnut, turned and pinned. Houses two flight controllers and PDB.

02

Arms × 6

Bamboo splint bundle, hexagonal-section, individually replaceable.

03

Tension members × 6

Hemp linen cord, bio-resin saturated. Redistributes rotor load.

04

Motor pods × 6

Walnut nacelles. Motor + ESC, replaceable as a unit.

05

Gimbal yoke

Bamboo and walnut. Pitch / roll / yaw, documented mount standard.

06

Battery tray

Hot-swap dual-bay. Either bay can sustain flight alone.

07

GPS mast

Bamboo dowel, RTK antenna integrated.

08

Landing legs × 4

Steam-bent bamboo, quick-release for transport.

  • inspection Wind turbine and bridge inspection — large standoff sensor work.
  • cinematography Heavy-camera aerial work, full-frame mirrorless and beyond.
  • logistics Remote-area medical and supply delivery — clinics, research stations.
  • research Atmospheric sampling, payload-heavy science work.

Vitruvius is currently in structural design. The frame has passed bench tests for static load and vibration; flight testing of the first prototype is scheduled for the third quarter of MMXXVI, with limited customer trials following six months later.

We are particularly interested in early partnerships with inspection contractors and cinematography houses where Vitruvius would replace a heavier, louder, less repairable machine.