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Pegna Bonmartini Rondine

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The Pegna-Bonmartini Rondine, or Pegna Rondine, is a single-seat ultralight sport aeroplane designed by Giovanni Pegna and built by Piaggio in Italy during 1923.

Contents

Development

Probably inspired by the success of entrants to the Lympne ultra-light aeroplane trials, Signore Pegna designed the Rondine to take advantage of small low-powered light weight engines available at the time.

Design

The Rondine is a mid-winged cantilever monoplane built primarily of wood with fabric-covered wings. The fuselage is noteworthy in being clinker or carvel built similar to boat building techniques. The single piece two-spar wings are of low aspect ratio and relatively thick so external bracing is unnecessary. Control is provided by conventional ailerons and rudder, with a small fixed fin and an all-flying tailplane and elevator mounted above the rear fuselage forward of the fin. The fixed undercarriage consists of braced trousered main legs and a tail-skid.

Several powerplants were tested with poor results until the 404 cc (24.65 cu in) ABC 8 hp, used successfully in other contemporary ultra-light aircraft, fitted with a 3:1 reduction gear, was found to be satisfactory.

Accommodation for the pilot is in an open cockpit, set at mid chord, with padded edges, protected from the slipstream by a three-piece windscreen.

Specifications (Rondine)

Data from Flight, 23 December 1923

General characteristics

  • Crew: 1
  • Length: 6 m (19 ft 8 in)
  • Wingspan: 10 m (32 ft 10 in)
  • Wing area: 20 m2 (220 sq ft)
  • Aspect ratio: 5
  • Empty weight: 131 kg (289 lb)
  • Gross weight: 211 kg (465 lb)
  • Powerplant: 1 × ABC 8hp 2-cyl. air-cooled horizontally opposed piston engine, 6.0 kW (8 hp)
  • Propellers: 2-bladed fixed pitch propeller with 3:1 reduction gearing
  • Performance

  • Maximum speed: 70 km/h (43 mph; 38 kn)
  • Landing speed: 40 km/h (25 mph; 22 kn)
  • Lift-to-drag: 14
  • References

    Pegna-Bonmartini Rondine Wikipedia