Engineering:Sportavia-Pützer SFS 31 Milan

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Short description: German motor glider, 1969
SFS 31 Milan
Scheibe SFS 31 Milan (8735473854).jpg
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), René Fournier (aircraft designer) (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

  • Crew: one pilot
  • Length: 6.05 m (19 ft 10 in)
  • Wingspan: 15.00 m (49 ft 3 in)
  • Height: 1.57 m (5 ft 2 in)
  • Wing area: 12.0 m2 (129 sq ft)
  • Aspect ratio: 18.6
  • Airfoil: Wortmann FX-61-184 at root, Wortmann FX-60-126 at tip
  • Empty weight: 310 kg (683 lb)
  • Gross weight: 440 kg (970 lb)
  • Powerplant: 1 × Rectimo 4 AR 1200 , 29 kW (39 hp)

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. Jump up to: 1.0 1.1 1.2 1.3 1.4 1.5 1.6 1.7 Taylor 1973, p.560
  2. Taylor 1989, p.838
  3. "Hanover Report", p.720
  4. Jump up to: 4.0 4.1 4.2 4.3 Hardy 1982, p.172
  5. Jump up to: 5.0 5.1 5.2 Hardy 1982, p.173
  6. Simpson 1995, p.378
  7. Ross 1971, p.14

References