Rahul Sharma (Editor)

SECAT RG 60

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Top speed
  
190 km/h

Length
  
4.95 m

Wingspan
  
5 m

The SECAT RG-60 was a prototype light sporting biplane built in France shortly after World War II. It was a conventional single-seat design with an open cockpit. The lower wing had a smaller span and chord than the upper wing and was braced against the upper wing and against the fuselage sides with I-struts but no wires. The undercarriage consisted of two fixed, divided main units plus a fixed tailskid. Power was supplied by a tractor-mounted piston engine that drove a two-bladed propeller. Construction was of wood throughout.

Contents

History

The RG-60 was displayed together with other SECAT designs at the Semaine de l'Aviation légère (light aviation week) held at Toussus-le-Noble from 22 April 1947 but was already somewhat outdated by the standards of the time. SECAT produced no further examples, and if the RG-60 ever received a civil registration, the details are now lost.

Specifications

Data from Jane's All The World's Aircraft 1948, except as noted

General characteristics

  • Crew: one pilot
  • Length: 4.95 m (16 ft 3 in)
  • Wingspan: 5.00 m (15 ft 5 in)
  • Height: 1.90 m (6 ft 3 in)
  • Wing area: 9.5 m2 (102 ft2)
  • Empty weight: 180 kg (397 lb)
  • Gross weight: 295 kg (650 lb)
  • Powerplant: 1 × Train 4A, 30 kW (40 hp)
  • Performance

  • Maximum speed: 190 km/h (118 mph)
  • Range: 500 km (311 miles)
  • Service ceiling: 5,000 m (16,400 ft)
  • References

    SECAT RG-60 Wikipedia