Roberts Cygnet

Cygnet
General information
TypeGlider
National origin
United States
Designer
StatusProduction completed
Number builtOne
History
First flight1992

The Roberts Cygnet is an American high-wing, cruciform tail, single-seat, glider that was designed and produced by Donald Roberts as a contender for the IGC World Class sailplane.

Design and development

The Cygnet was the sole US entrant in the competition for the World Class sailplane, losing out to the Polish Politechnika Warszawska PW-5. As a result, only one Cygnet was completed. The prototype was finished and first flown in 1992

The aircraft is made from steel tubing and aluminium, with fiberglass fairings. Its 13 m (42.7 ft) span wing employs a Somers-Maughmer SM701 airfoil and features balanced top and bottom DFS-style air brakes for glidepath control. A ballistic parachute was to be standard equipment.

Operational history

In August 2011 the sole Cygnet built was still listed on the US Federal Aviation Administration registry.

Specifications (Cygnet)

Data from Sailplane Directory

General characteristics

Performance

See also

Related lists

References

  1. 1 2 3 4 Activate Media (2006). "Cygnet Roberts". Archived from the original on September 2, 2012. Retrieved August 25, 2011.
  2. ↑ Lednicer, David (2010). "The Incomplete Guide to Airfoil Usage". Archived from the original on July 19, 2011. Retrieved August 1, 2011.
  3. ↑ Federal Aviation Administration (August 2011). "Make / Model Inquiry Results". Retrieved August 15, 2011.