Abraham Iris

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, and the Iris II with a Renault engine. 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)

See also

Related lists

• List of utility aircraft