Der Dessauer
Der Dessauer | |
---|---|
![]() | |
Role | Single seat glider |
National origin | Germany |
Manufacturer | Flugtechnischer Verein, Dessau |
Designer | Ludwig Hoffmann |
First flight | 1923 |
Number built | 1 |
The Der Dessauer, later Der alte Dessauer, was a German single-seat
Design and development
Around 1923, Ludwig Hoffmann was a Junkers employee and co-founder of the Flugtechnische Verein Dessau (Flight Technical Association Dessau). He had already had experience in glider design at Akaflieg Darmstadt with the Akaflieg Darmstadt D-6 Geheimrat. The Der Dessauer was recognisable as a descendant of that glider.[1][2]
The Der Dessauer was a
The Der Dessauers fuselage was wood-framed and skinned with plywood. There were no internal cross frames; instead the ply skin carried the stresses.
Operational history
The Der Dessauer was a competitor at the 1923 Rhön (Wasserkuppe) competition; though it did not win it, pilot Otto Thomsen used its manoeuvrability, particularly in circling, to advantage.[1][4] On the last day of the contest, 30 August, a crowd of about 30,000 people gathered to observe the dedication of a memorial to those glider pilots who had died on the Wasserkuppe. Despite very gusty conditions, several gliders flew and some crashed; amongst these was Der Dessauer. Violent wing oscillations set in and although Thomsen was able to bring the aircraft down before the wings broke away, the impact very seriously damaged it. The accident was blamed upon resonances caused by the elastic wing struts. Thomsen was not seriously hurt.[1]
Despite the damage, the Der Dessauer was rebuilt by a small group at the
It continued to fly competitively for three more years, attending all the Rhön events from 1925 to 1928, frequently flown by Akaflieg Dessau students, one of whom irreparably damaged it there in 1928.[1]
Specifications
Data from Historische Deutsche Flugzeug p.23.[1] Weights and performance figures are approximate
General characteristics
- Crew: One
- Length: 6.10 m (20 ft 0 in)
- Wingspan: 12.80 m (42 ft 0 in)
- Height: 1.35 m (4 ft 5 in)
- Wing area: 15.5 m2 (167 sq ft)
- Aspect ratio: 10.57
- Airfoil: Göttingen 289
- Empty weight: 100 kg (220 lb)
- Gross weight: 176 kg (388 lb)
- Wing loading: 11.5 kg/m2 (2.4 lb/sq ft)
Performance
- Maximum speed: 140 km/h (87 mph, 76 kn)
- Minimum control speed: 40 km/h (25 mph, 22 kn)
- Maximum glide ratio: best, 1:19
- Rate of sink: 0.6 m/s (120 ft/min)
See also
References
- ^ ISBN 978-3-923142-39-2.
- ISBN 3 9806773 4 6.
- ^ a b "Gliders in Germany". Popular Aviation. July 1928. p. 58.
- ^ a b Pagé, Victor (1930). A B C of Gliding and Sailflying. New York: Norman W. Henley Publishing Co. pp. 88–91.
External links
![](http://upload.wikimedia.org/wikipedia/en/thumb/4/4a/Commons-logo.svg/30px-Commons-logo.svg.png)