Since the aircraft is still currently undergoing development and testing, some of the information contained on this page is still in the form of feasible projections and probabilities, based on design-specific calculations.

Once the test-flight program is completed, all technical and performance specifications will be reviewed and, where required, revised accordingly!

Side View + Design

Dimensional analysis

Dimensions

Width: 1.9 m
Length: 4.8 m
Height: 3.2 m

Mod06

Weight & Capacity

Basic empty weight: 280 Kg
Typical operating weight: 550 Kg
Special purpose operations (MAUW): 650 Kg

 

Instrumentation

Standard VFR instruments, intercom and radio communications.

 

Undercarriage

Wheel base: 1.9 m
Track: 1.7 m
Main wheels: 5.00-5, 6 ply
Nose wheel: 5.00-5, 6 ply

 

Rotor

Extruded aluminium 240 mm chord
Length: 8.8 m – 9.5 m (≈ 29′ – 31′)
Airfoil profile: NACA 8-H-12

 

Power Plant

100_7703

UL 350 i

UL Power 350i FADEC FHI EJ 25: Auto-Aero Conversion
Power Output: 118 hp, normally aspirated 170 hp, normally aspirated
Capacity: 3 500 cc, fuel injected 2 500 cc, fuel injected
Configuration: 4 cylinders, horizontally opposed, air-cooled 4 cylinders, horizontally opposed, liquid-cooled

 

Lubricants and Fuel

Engine Oil: 15W40 semi-synthetic
Fuel Tank: 75 litres (70 litres usable)
Type of fuel: MoGas 95 Unleaded or AvGas 100LL (within specified limits)
Fuel consumption: 20 ℓ / hr @ cruise power setting.

 

Projected Performance

Mod02

Nacelle / cowling / frame / engine interfacing

Never exceed airspeed: (VNE) 125 mph / 200 km/h
Maximum level-flight airspeed: (VH) 110 mph / 176 km/h
Cruising airspeed: 100 mph / 160 km/h
Minimum airspeed: (Straight and Level, no wind): 30 mph / 48 km/h
Rotor RPM: 340 to 350 RPM
Service ceiling: > 10 000 ft / 3 050 m
Take-off distance: (No wind, 210 RPM pre-rotation) 150 m
Landing-roll: 0 – 10 m
Endurance: 3 hours with 30 minute reserves.