Milomei M2
| Milomei M2 | |
|---|---|
| Type: | Glider |
| Design country: | |
| Manufacturer: |
Michael-Lorenz Meier |
| First flight: |
April 7, 1981 |
| Number of pieces: |
1 |
The Milomei M2 is a single-seat glider with variable wing geometry . The competition number is M2, the number D-2502.
History and construction
The aircraft designed by Michael-Lorenz Meier and built as a single piece flew for the first time on April 7, 1981.
The self-supporting shoulder wing with normal tail unit is a light metal construction in a shell construction. The rectangular trapezoidal wing has two spar webs, a spoiler and flaps and is clad with 0.6 mm foam-supported duralumin . The wing with the modified Wortmann profile can be enlarged by extending a Wortmann flap from the rear edge over the entire span by 4.4 m² to 16.6 m². There are surface wheels on the edge arches.
The fuselage with unsprung retractable landing gear and braking parachute is clad with 0.8 mm aluminum sheet. The cockpit canopy consists of a fixed and a pluggable part made of acrylic glass . The tail unit with pendulum elevator and rudder with tubular steel spars and foam core is also metal-clad.
Technical specifications
| Parameter | Data |
|---|---|
| crew | 1 |
| length | 7.85 m |
| span | 22.00 m |
| height | |
| Wing profile | Wortmann FX 67-VC-170/136 |
| Wing area | 12.2-16.6 m² |
| Elongation | 36.67-29.16 |
| Glide ratio (arithmetical) | 49 at 95 km / h |
| Slightest sinking | 0.50 m at 65 km / h |
| Preparation mass | 365 kg |
| Max. Takeoff mass | 510 kg |
| Minimum speed | 77 km / h |
| Top speed | 290 km / h |
See also
Individual evidence
- ↑ Type description Milomei M2. In: segelflug.de. Retrieved December 25, 2018 .