Abraham Iris
| Abraham Iris | |
|---|---|
| Role | Touring aircraft |
| Manufacturer | Abraham |
| Produced | 1930s |
The Abraham Iris was a two-seat touring airplane produced in France in the early 1930s in two slightly different versions, the Iris I with a 75 kW (100 hp) Hispano-Suiza piston engine,[1] and the Iris II with a Renault engine.[2] The Iris was a conventional parasol wing monoplane with a neatly faired-in engine.
Specifications (Iris II)
General characteristics
- Crew: 1
- Capacity: 1 passenger
- Length: 6.87 m (22 ft 6 in)
- Wingspan: 9.80 m (32 ft 2 in)
- Height: 2.50 m (7 ft 7 in)
- Wing area: 15 m² (161 ft²)
- Empty weight: 467 kg (1,027 lb)
- Loaded weight: 760 kg (1,672 lb)
- Powerplant: 1 × Renault 4Pb, 71 kW (95 hp)
Performance
- Maximum speed: 180 km/h (98 knots, 113 mph)
- Range: 400 km (220 nm, 250 mi)
- Wing loading: 51 kg/m² (10 lb/ft²)
- Power/mass: 90 W/kg (0.06 hp/lb)
References
External links
This article is issued from
Wikipedia.
The text is licensed under Creative Commons - Attribution - Sharealike.
Additional terms may apply for the media files.