Oberlerchner Mg 23
Mg 23 | |
---|---|
Musger Mg 23 (OE-0425) at the Aviaticum museum | |
Role | Single seat high performance sailplane |
National origin | Austria |
Manufacturer | Josef Oberlerchner Holzindustrie, Spittal an der Drau |
Designer | Erwin Musger |
First flight | 25 June 1955 (Mg 23 prototype) |
Number built | 26 by March 1966, including prototypes |
The Oberlerchner Mg 23 is a single-seat, all-wood, high-performance sailplane. It was built and first flown in Austria in 1955, and a total of 26 were built before production ended in 1965.
Design and development
The Mg 23, an Erwin Musger design often known as the Musger Mg 23, was an all-wood
The fuselage had an oval section of wooden semi-monocoque construction, tapering to the rear. On the production SL the fuselage line over the wings merged into a forward-sliding canopy, which was longer than that of the prototype. The Mg 23 SL had a fixed monowheel undercarriage, and both integral nose- and tailskids.[1]
The Mg 23 prototype flew on 25 June 1955, flight testing leading to the increase in vertical tail size and a modified canopy on the production aircraft, the first of which was flown on 1 April 1962.[1]
Operational history
26 Mg 23 SLs had been built by March 1966. In mid-2010, 11 Mg 23s were on the civil registers of European countries, nine in Austria, one in Switzerland and one in the Netherlands.[2] Three were exported to the United States and one to Canada.[3]
Aircraft on display
An Mg 23, one of those still on the Austrian register, is on display in the Flugmuseum Aviaticum, Wiener Neustadt-Ost, Austria[4]
- Western Antique Aeroplane & Automobile Museum Has a 1964 mg-23SL .
Variants
- Mg 23
- Prototype, eight built.
- Mg 23 SL
- Production model, 18 built.
Specifications (Mg 23)
Data from Jane's All the World's Aircraft 1966/7 and The World's Sailplanes:Die Segelflugzeuge der Welt:Les Planeurs du Monde.[1][5]
General characteristics
- Crew: one
- Length: 7.11 m (23 ft 4 in) (Mg 23SL 7.22 m (23 ft 8 in)
- Wingspan: 16.40 m (53 ft 10 in)
- Height: 1.49 m (4 ft 11 in)
- Wing area: 14.21 m2 (153.0 sq ft)
- Aspect ratio: 18.54
- Airfoil: NACA63.015(Mg 23SL - NACA63 1315)
- Empty weight: 240 kg (529 lb)
- Max takeoff weight: 360 kg (794 lb)
Performance
- Stall speed: 60 km/h (37 mph, 32 kn)
- Never exceed speed: 180 km/h (110 mph, 97 kn) smooth air (Mg 23SL - 220 km/h (137 mph; 119 kn)
- Rough air speed max: 130 km/h (81 mph; 70 kn)
- Aerotow speed: 130 km/h (81 mph; 70 kn)
- Winch launch speed: 80 km/h (50 mph; 43 kn)
- g limits: +4 at 216 km/h (134 mph; 117 kn)
- Maximum glide ratio: 32:1 at 79 km/h (49 mph; 43 kn)
- 33:1 at 85 km/h (53 mph; 46 kn)
- Rate of sink: 0.66 m/s (130 ft/min) minimum, at 68 km/h (42 mph; 37 kn)
- (Mg 23SL 0.68 at 78 km/h (48 mph; 42 kn)
- Wing loading: 25.3 kg/m2 (5.2 lb/sq ft)
References
- ^ a b c d Taylor, John W R (1966). Jane's All the World's Aircraft 1966-67. London: Sampson Low, Marston & Co. Ltd. p. 382.
- ISBN 978-0-7106-2916-6.
- ISBN 3-900368-10-4.
- ^ "Mg 23 on display in Vienna". Retrieved 2011-01-16.
- ^ Shenstone, B.S.; K.G. Wilkinson; Peter Brooks (1958). The World's Sailplanes:Die Segelflugzeuge der Welt:Les Planeurs dans Le Monde (in English, French, and German) (1st ed.). Zurich: Organisation Scientifique et Technique Internationale du Vol a Voile (OSTIV) and Schweizer Aero-Revue. pp. 9–13.
External links
Media related to Oberlerchner Mg 23 at Wikimedia Commons