Young Skyheater

From Wikipedia, the free encyclopedia

This is an old revision of this page, as edited by Citation bot (talk | contribs) at 09:07, 23 August 2019 (Add: journal. Removed parameters. Some additions/deletions were actually parameter name changes.| You can use this bot yourself. Report bugs here.| Activated by User:Chris Capoccia | Category:Pages with citations lacking titles.). The present address (URL) is a permanent link to this revision, which may differ significantly from the current revision.

Skyheater
Role Homebuilt aircraft
National origin United States
Designer Ed Young

The Young Skyheater is an American aircraft that was designed by Ed Young for homebuilt construction.

Design and development

The Skyheater is a two-seat, single engine, conventional landing gear-equipped, parasol wing aircraft. Rather than a separate distinct vertical tail section, the Skyheater fuselage is tapered only along its sides, leaving a square tail or full-height dorsal fin extending to the wing root. The fuselage is constructed of welded steel tubing with fabric covered control surfaces. The wings are of all aluminum construction.[1]

Specifications (Young Skyheater)

Data from Air Progress

General characteristics

  • Crew: 1
  • Capacity: 1
  • Length: 21 ft (6.4 m)
  • Wingspan: 28 ft (8.5 m)
  • Powerplant: 1 × Continental O-300 horizontally-opposed piston engine, 145 hp (108 kW)
  • Propellers: 2-bladed

See also

Aircraft of comparable role, configuration, and era

References

  1. ^ Air Progress: 9. Winter 1969. {{cite journal}}: Missing or empty |title= (help)