Engineering:Albatros L 60
From HandWiki
| L 60 | |
|---|---|
| Role | Utility aircraft |
| Manufacturer | Albatros Flugzeugwerke |
| First flight | 1923 |
| Produced | 3 |
The Albatros L 60 was a two-seat Germany utility aircraft of the 1920s developed from the Albatros L 59. It was a single-engine low-wing cantilever monoplane with large, spatted undercarriage.
Specifications (L 60)
General characteristics
- Crew: one pilot
- Capacity: 1 passenger
- Length: 5.40 m (17 ft 9 in)
- Wingspan: 10.30 m (33 ft 9 in)
- Height: 2.65 m (8 ft 8 in)
- Wing area: 10.0 m2 (108 sq ft)
- Empty weight: 369 kg (814 lb)
- Gross weight: 600 kg (1,323 lb)
- Powerplant: 1 × Siemens-Halske Sh 5 , 60 kW (80 hp)
Performance
- Maximum speed: 165 km/h (100 mph, 87 kn)
- Range: 400 km (250 mi, 220 nmi)
- Service ceiling: 3,000 m (9,800 ft)
- Rate of climb: 2.1 m/s (410 ft/min)
See also
References
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. pp. 55.
- German Aircraft between 1919–1945
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