From Wikipedia, the free encyclopedia
(Redirected from Sportavia Milan)
SFS 31 Milan
SFS 31
Role Motor glider
National origin Germany
Manufacturer Sportavia-Pützer [ de]
Scheibe Flugzeugbau
First flight 31 August 1969 [1]
Number built 14 by 1973 [1]
Developed from Fournier RF 4
Scheibe SF-27

The Sportavia-Pützer SFS 31 Milan is a single-seat motor glider that was produced in Germany in the early 1970s.

Design and development

The Milan was created by essentially combining the fuselage of the Fournier RF 4 with the wings of the Scheibe SF-27. [2] [3] [4] The resulting aircraft is a conventional motorglider design, a low-wing cantilever monoplane with a nose-mounted engine. [1] [4] The undercarriage consists of a single retractable mainwheel, a fixed tailwheel, and an outrigger under each wing. [1] [5] Construction is of wood, skinned in plywood and fabric. [1] [5] The designation was created by combining the initials of the manufacturers involved ( Sportavia-Pützer [ de], Fournier [ fr] , and Scheibe), and adding the sum of the model numbers of the two constituent aircraft designs. [1] [4]

The SFS 31 prototype (registered D-KORO) first flew on 31 August 1969 [1] [4] and soon replaced the RF 4D in production at Sportavia-Pützer. [6] In 1971, Hans Huth piloted an SFS 31 to third place in the German national motorglider competition. [1] [7]

Specifications

Data from Taylor 1977, p.560, except as noted

General characteristics

Performance

  • Cruise speed: 180 km/h (112 mph, 97 kn)
  • Range: 670 km (415 mi, 361 nmi)
  • Service ceiling: 6,000 m (19,700 ft)
  • Maximum glide ratio: 29:1 [5]
  • Rate of climb: 3.0 m/s (590 ft/min)

Notes

  1. ^ a b c d e f g h Taylor 1973, p.560
  2. ^ Taylor 1989, p.838
  3. ^ "Hanover Report", p.720
  4. ^ a b c d Hardy 1982, p.172
  5. ^ a b c Hardy 1982, p.173
  6. ^ Simpson 1995, p.378
  7. ^ Ross 1971, p.14

References

  • Hardy, Michael (1982). Gliders & Sailplanes of the World. London: Ian Allan.
  • "Hanover Report". Flight International: 713–22. 30 April 1970. Retrieved 2011-03-13.
  • Ross, Peter (1 July 1971). "Soaring to Power". Flight International: 14–15. Retrieved 2011-03-13.
  • Simpson, R.W. (1995). Airlife's General Aviation. Shrewsbury: Airlife.
  • Taylor, John W.R. (1974). Jane's All the World's Aircraft 1973–74. London: Jane's Yearbooks.
  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions.
From Wikipedia, the free encyclopedia
(Redirected from Sportavia Milan)
SFS 31 Milan
SFS 31
Role Motor glider
National origin Germany
Manufacturer Sportavia-Pützer [ de]
Scheibe Flugzeugbau
First flight 31 August 1969 [1]
Number built 14 by 1973 [1]
Developed from Fournier RF 4
Scheibe SF-27

The Sportavia-Pützer SFS 31 Milan is a single-seat motor glider that was produced in Germany in the early 1970s.

Design and development

The Milan was created by essentially combining the fuselage of the Fournier RF 4 with the wings of the Scheibe SF-27. [2] [3] [4] The resulting aircraft is a conventional motorglider design, a low-wing cantilever monoplane with a nose-mounted engine. [1] [4] The undercarriage consists of a single retractable mainwheel, a fixed tailwheel, and an outrigger under each wing. [1] [5] Construction is of wood, skinned in plywood and fabric. [1] [5] The designation was created by combining the initials of the manufacturers involved ( Sportavia-Pützer [ de], Fournier [ fr] , and Scheibe), and adding the sum of the model numbers of the two constituent aircraft designs. [1] [4]

The SFS 31 prototype (registered D-KORO) first flew on 31 August 1969 [1] [4] and soon replaced the RF 4D in production at Sportavia-Pützer. [6] In 1971, Hans Huth piloted an SFS 31 to third place in the German national motorglider competition. [1] [7]

Specifications

Data from Taylor 1977, p.560, except as noted

General characteristics

Performance

  • Cruise speed: 180 km/h (112 mph, 97 kn)
  • Range: 670 km (415 mi, 361 nmi)
  • Service ceiling: 6,000 m (19,700 ft)
  • Maximum glide ratio: 29:1 [5]
  • Rate of climb: 3.0 m/s (590 ft/min)

Notes

  1. ^ a b c d e f g h Taylor 1973, p.560
  2. ^ Taylor 1989, p.838
  3. ^ "Hanover Report", p.720
  4. ^ a b c d Hardy 1982, p.172
  5. ^ a b c Hardy 1982, p.173
  6. ^ Simpson 1995, p.378
  7. ^ Ross 1971, p.14

References

  • Hardy, Michael (1982). Gliders & Sailplanes of the World. London: Ian Allan.
  • "Hanover Report". Flight International: 713–22. 30 April 1970. Retrieved 2011-03-13.
  • Ross, Peter (1 July 1971). "Soaring to Power". Flight International: 14–15. Retrieved 2011-03-13.
  • Simpson, R.W. (1995). Airlife's General Aviation. Shrewsbury: Airlife.
  • Taylor, John W.R. (1974). Jane's All the World's Aircraft 1973–74. London: Jane's Yearbooks.
  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions.

Videos

Youtube | Vimeo | Bing

Websites

Google | Yahoo | Bing

Encyclopedia

Google | Yahoo | Bing

Facebook