Av8er Orbiter

Design and development

The Orbiter was designed to comply with the US FAR 103 Ultralight Vehicles rules as well as European regulations. It features a paraglider-style wing, single-place accommodation and a single engine in pusher configuration. The aircraft is built with special attention to balancing and vibration isolation. The cage assembly includes small wheels to ease ground movement of the motor unit.

As is the case with all paramotors, take-off and landing is accomplished by foot. Inflight steering is accomplished via handles that actuate the canopy brakes, creating roll and yaw.

Variants

Orbiter Lite

Model with a 14 hp (10 kW) Radne Raket 120 Aero ES engine in pusher configuration with a 4:1 ratio reduction drive and a 140 cm (55 in) diameter two-bladed wooden propeller. The fuel tank capacity is 10 litres (2.2 imp gal; 2.6 US gal).

Orbiter XP

Base model circa 2005.

Orbiter XPE

Model with electronic starting.

Orbiter XPR Light

Model with Radne Raket 120 engine.

Specifications (Orbiter Lite)

Data from Bertrand

General characteristics

Crew: one

Empty weight: 20 kg (44 lb)

Fuel capacity: 10 litres (2.2 imp gal; 2.6 US gal)

Powerplant: 1 × Radne Raket 120 Aero ES single cylinder, two-stroke, air-cooled aircraft engine, with a 4:1 reduction drive, 10 kW (14 hp)

Propellers: 2-bladed wooden, fixed pitch, 1.40 m (4 ft 7 in) diameter