Neukom Elf 17a
Elf 17a | |
---|---|
Type: | Glider |
Design country: | |
Manufacturer: |
Albert Neukom |
First flight: |
1973 |
The Elfe 17a is a wooden / composite construction glider that was built in the early 1970s.
It was designed by the Swiss architect Albert Neukom , who has developed and built numerous gliders since the mid-1950s. A mix of materials for various components on the aircraft is typical of Neukom's designs. In the Elfe 17, for example, the wing spar is made of aluminum and the hull is made of plywood. The glide ratio of 40 is comparable to that of gliders in GRP construction .
The cantilevered shoulder wing with cross tail, pendulum rudder and a rudder with compensation surface has a retractable canopy and retractable landing gear .
Technical specifications
Parameter | Data |
---|---|
crew | 1 |
length | 7.30 m |
span | 17.00 m |
Elevation (rudder) | 1.80 m |
mean chord (geometric) | 0.783 m |
mean chord (aerodynamic) | 0.817 m |
Wing pitch angle to rear fuselage axis | + 3 ° |
Wing area | 13.3 m² |
Wing extension | 22nd |
Wing profile | Wortmann , from FX 61-163 to FX 60-126 |
Glide ratio | 38-40.5 |
Preparation mass | 270 kg |
Max. Takeoff mass | 380 kg |
Wing loading | 28.6 kg / m² |
Top speed | 180 km / h |
Web links
Commons : Neukom Elfe - Collection of images, videos and audio files
- Technical data and flight behavior of the Elfe aircraft
- Neukom S-4 Elfe 17 on www.j2mcl-planeurs.net (English)
Individual evidence
- ↑ J2mcL Planeurs - Fiche planeur n °. Retrieved May 18, 2020 .
- ↑ Elf 17m. In: www.segelflug.de. Retrieved May 18, 2020 .