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,[1] and the Iris II with a Renault engine.[2] The Iris was a conventional parasol wing monoplane with a neatly faired-in engine.

Abraham Iris
Role Touring aircraft
Manufacturer Abraham
Produced 1930s

Specifications (Iris II)

Data from Aviafrance : Abraham AS-2 'Iris' II[2]

General characteristics

  • Crew: 2
  • Length: 6.87 m (22 ft 6 in)
  • Wingspan: 9.8 m (32 ft 2 in)
  • Height: 2.5 m (8 ft 2 in)
  • Empty weight: 467 kg (1,030 lb)
  • Gross weight: 760 kg (1,676 lb)
  • Powerplant: 1 × Renault 4Pb 4-cylinder air-cooled in-line piston engine, 71 kW (95 hp)
  • Propellers: 2-bladed fixed-pitch propeller

Performance

  • Maximum speed: 180 km/h (110 mph, 97 kn)
  • Range: 400 km (250 mi, 220 nmi)
  • Wing loading: 51 kg/m2 (10 lb/sq ft)
  • Power/mass: 0.099 kW/kg (0.06 hp/lb)
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References
  1. Parmentier, Bruno (12 January 2004). "Abraham AS-2 'Iris' I". Avuiafrance (in French). Retrieved 15 June 2020.
  2. Parmentier, Bruno (20 April 2000). "Abraham AS-2 'Iris' II". Avuiafrance (in French). Retrieved 15 June 2020.
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