A | B | C | D | E | F | G | H | CH | I | J | K | L | M | N | O | P | Q | R | S | T | U | V | W | X | Y | Z | 0 | 1 | 2 | 3 | 4 | 5 | 6 | 7 | 8 | 9
| Darmstadt D-29 | |
|---|---|
| |
| Role | Experimental cabin monoplane |
| National origin | Germany |
| Manufacturer | Akaflieg Darmstadt |
| First flight | 1936 |
| Produced | 1936 |
| Number built | 1 |
The Darmstadt D-29 was a German experimental monoplane designed and built by Akaflieg Darmstadt (of the Darmstadt University of Technology). The D-29 was a cantilever low-wing monoplane designed and built during 1936 with a conventional landing gear with a tailskid. It was powered by a Siemens-Halske Sh 14a radial piston engine and had enclosed tandem cockpits, as well as a number of other features, including hydraulically actuated trailing-edge flaps, a braced T-tail and leading-edge slots.
Specifications
Data from Illustrated Encyclopedia of Aircraft[1]
General characteristics
- Crew: 2
- Length: 7.10 m (23 ft 4 in)
- Wingspan: 8.80 m (28 ft 10 in)
- Height: 2.75 m (9 ft 0 in)
- Wing area: 10.00 m2 (107.6 sq ft)
- Empty weight: 560 kg (1,235 lb)
- Max takeoff weight: 850 kg (1,874 lb)
- Powerplant: 1 × Siemens-Halske Sh 14a radial piston engine, 110 kW (150 hp)
Performance
- Maximum speed: 245 km/h (152 mph, 132 kn)
- Range: 675 km (419 mi, 364 nmi)
References
Notes
- ^ Orbis 1985, p. 1313
Bibliography
- The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing.
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