Akaflieg Munich Mü 30
| Akaflieg Munich Mü 30 "Schlacro" | |
|---|---|
|
|
| Type: | Artificial and towing aircraft |
| Design country: | |
| Manufacturer: | |
| First flight: |
June 16, 2000 |
| Commissioning: |
November 29, 2011 |
| Number of pieces: |
1 |
The Akaflieg München Mü 30 "Schlacro" ( Schl epp and Acro aircraft) of the student flying group Akaflieg München is a two-seat aerobatic aircraft (Acro) that can be used for aircraft towing .
history
Development started in 1985. Production of the planned Porsche PFM 3200 engine was discontinued in 1990, so that after the first fuselage parts had been completed, the Lycoming AEIO 540 L1B5D six-cylinder boxer engine with 223 kW was changed. The design changes required for this, such as moving the wings 150 mm forward to achieve the desired center of gravity, delayed completion. The first flight took place in 2000. The flight test was interrupted in particular due to problems with the engine cooling and finally continued in 2007 after modifications. In November 2011, the final traffic approval by the Luftfahrt-Bundesamt followed .
construction
The Mü 30 is a two - seater low - wing aircraft that is controlled from the rear seat. The fuselage consists of welded steel pipes that are clad with fiber composite parts . The wings with a span of 8.96 meters are made of carbon fiber reinforced plastic (CFRP) . The structure is designed for a load multiple of +/− 9 g and has a curb weight of 759 kg.
use
The Mü 30 "Schlacro" with the registration D-EKDF is used by Akaflieg Munich at the Königsdorf glider airfield as a towing aircraft for gliders . The aircraft takes part in aerobatic competitions as well as national and international trade fairs, such as the International Aerospace Exhibition Berlin (ILA) since 2008 .
Technical specifications
| Parameter | Data |
|---|---|
| crew | 1 |
| Passengers | 1 |
| length | 7.40 m |
| span | 8.96 m |
| height | 2.90 m |
| Wing area | 11.96 m² |
| Wing extension | 6.5 |
| best glide ratio | 7 at 75 kt (139 km / h) |
| Max. Climb performance | 2600 ft / min (13.2 m / s) |
| payload | 291 kg |
| Empty mass | 759 kg |
| Takeoff mass | 1050 kg |
| permissible load multiples | +/- 9 g |
| Take-off run | 124 m |
| Stall speed | 48 kt (89 km / h) |
| Cruising speed | 145 kt (269 km / h) at 75% power |
| Top speed | 212 kt (393 km / h) |
| Service ceiling | 10,000 ft (3048 m) |
| Max. Amount of fuel | 189 l in three tanks |
| Max. Range | 389 NM (720 km) |
| Engines | 1 Lycoming AEIO-540-L1B5D , 223 kW (300 hp) |
| fuel | AvGas 100LL |
| Displacement | 540 cuin (8875 cm³) |
| propeller | MT Propeller MTV-14, Constant Speed , diameter 1.90 m |
See also
literature
- Paul Jackson: Jane's All the World's Aircraft 2001-2002 . Jane's Information Group , 2001, ISBN 978-0-7106-2307-2 .
Web links
Individual evidence
- ↑ Lexicon of Aircraft by Wolfgang Bredow , accessed on December 15, 2016
- ↑ Kyrill von Gersdorff, Helmut Schubert, Kurt Grasmann, Stefan Ebert, Richard Faltermair: Aircraft engines and jet engines. Development history of German aviation engines from the beginnings to the international joint developments. Bernard & Graefe, Koblenz 2007, ISBN 3-7637-5283-8 , p. 222.
- ↑ Project page of the Mü 30 "Schlacro" on the Akaflieg Munich website , accessed on December 15, 2016
- ↑ Flight manual of the Mü 30 "Schlacro" D-EKDF, section 1
Gliders: Mü 1 “Vogel Roch” | Mü 2 “Münchner Kindl” | Mü 3 "Cockatoo" | Mü 4 "Munich" | Mü 5 "Wastl" | Mü 6 | Mü 10 "Milan" | Mü 11 "Parrot" | Mü 12 "Kiwi" | Mü 13 "Merlin" | Mü 15 | Mü 17 "Merle" | Mü 18 “Measuring crow” | DM-1 | Mü 22 | Mü 26 | Mü 27 | Mü 28 | Mü 31 | Mü 32 "ripping master"
Motor sailer: Mü 13 "Motormerlin" | Mü 23 "Saurian"
Motorized aircraft: Mü 8 | Mü 30 "Schlacro"