Rahul Sharma (Editor)

Abraham Iris

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Top speed
  
180 km/h

Length
  
6.87 m

Wingspan
  
9.8 m

Manufacturer
  
Abraham

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)

    • References

    Abraham Iris Wikipedia
    (Text) CC BY-SA