Houde Bimax
French ultralight aircraft
From Wikipedia, the free encyclopedia
The Houde Bimax is a French ultralight aircraft, designed and produced by Patrice Houde, introduced at the Blois homebuilt aircraft fly-in in September 2010. The aircraft is supplied as a complete ready-to-fly-aircraft.[1][2]
| Bimax | |
|---|---|
| General information | |
| Type | Ultralight aircraft |
| National origin | France |
| Manufacturer | Patrice Houde |
| Designer | Patrice Houde |
| Status | In production (2011) |
| History | |
| Introduction date | September 2010 |
Design and development
The Bimax was designed to comply with the Fédération Aéronautique Internationale microlight rules. It features a cantilever low-wing, a two-seats-in-tandem enclosed cockpit under a bubble canopy, fixed conventional landing gear and a single engine in tractor configuration.[1][2]
The aircraft is made from wood, with its flying surfaces covered in doped aircraft fabric. Its 8.25 m (27.1 ft) span wing is detachable for ground transportation and storage. Standard engines available are the 80 hp (60 kW) Rotax 912UL and the 100 hp (75 kW) Rotax 912ULS four-stroke powerplants.[1][2]
Specifications (Bimax)
Data from Bayerl and Tacke[1][2]
General characteristics
- Crew: one
- Capacity: one passenger
- Wingspan: 8.25 m (27 ft 1 in)
- Empty weight: 278 kg (613 lb)
- Gross weight: 472.5 kg (1,042 lb)
- Fuel capacity: 110 litres (24 imp gal; 29 US gal)
- Powerplant: 1 × Rotax 912UL four cylinder, liquid and air-cooled, four stroke aircraft engine, 60 kW (80 hp)
Performance
- Maximum speed: 250 km/h (160 mph, 130 kn)
- Cruise speed: 210 km/h (130 mph, 110 kn)
- Stall speed: 64 km/h (40 mph, 35 kn)
- Never exceed speed: 280 km/h (170 mph, 150 kn)