Engineering:Scheibe SF-24 Motorspatz

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Short description: German motor glider, 1960
SF-24 Motorspatz
General information
TypeMotor glider
National originWest Germany
ManufacturerScheibe Flugzeugbau
Designer
Number built50
History
Introduction date1960
First flight1960
Developed fromScheibe Spatz

The Scheibe SF-24 Motorspatz (English: Motor Sparrow) is a West German high-wing, single-seat motor glider that was designed by Egon Scheibe and produced by Scheibe Flugzeugbau.[1][2]

Derived from the unpowered Scheibe Spatz, the Motor Spatz was described in 1983 by Soaring Magazine as "one of the more primitive of the breed of self-launching sailplanes".

Design and development

The Motorspatz was an early attempt to create a self-launching glider. Scheibe accomplished this by mounting a Hirth engine in the nose of a mostly stock Spatz glider.[1][2]

The SF-24 is constructed with a welded steel tube fuselage that mounts the monowheel landing gear, with a small tail wheel for ground maneuvering. The wings and tail surfaces are built with wooden structures and covered in doped aircraft fabric covering. The wing has a 14.0 m (46 ft) span, employs an Mu 14% airfoil and mounts spoilers for glidepath control.[1][2][3]

The aircraft was not type certified and 50 were built.[1][2]

Operational history

In July 2011 there were two Motorspatz registered in the United States with the Federal Aviation Administration, including one SF-24 in the Experimental - Exhibition category and one SF-24B in the Experimental - Research and Development category.[4]

Variants

SF-24
Initial version[1][2]
SF-24A
Improved version[1][2]
SF-24B
Improved version[1][2]

Specifications (SF-24)

Data from Sailplane Directory and Soaring[1][2]

General characteristics

  • Crew: one
  • Wingspan: 14 m (45 ft 11 in)
  • Wing area: 11.87 m2 (127.8 sq ft)
  • Airfoil: Mu 14%
  • Empty weight: 225 kg (496 lb)
  • Gross weight: 345 kg (761 lb)
  • Powerplant: 1 × Hirth

Performance

  • Rate of sink: 1.0 m/s (200 ft/min) at 80 km/h (50 mph)
  • Wing loading: 29.21 kg/m2 (5.98 lb/sq ft)

See also

References

  1. ↑ 1.0 1.1 1.2 1.3 1.4 1.5 1.6 1.7 Activate Media (2006). "Motorspatz SF-24 Scheibe". Archived from the original on 29 August 2012. https://web.archive.org/web/20120829145312/http://www.sailplanedirectory.com/PlaneDetails.cfm?PlaneID=233. Retrieved 29 July 2011. 
  2. ↑ 2.0 2.1 2.2 2.3 2.4 2.5 2.6 2.7 Said, Bob: 1983 Sailplane Directory, Soaring Magazine, page 126. Soaring Society of America, November 1983. USPS 499-920
  3. ↑ Lednicer, David (2010). "The Incomplete Guide to Airfoil Usage". http://www.ae.illinois.edu/m-selig/ads/aircraft.html. Retrieved 1 July 2011. 
  4. ↑ Federal Aviation Administration (July 2011). "Make / Model Inquiry Results". http://registry.faa.gov/aircraftinquiry/AcftRef_Results.aspx?Mfrtxt=&Modeltxt=SF-24&PageNo=1. Retrieved 29 July 2011. 

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