Albatros L 68
The Albatros L 68 Alauda was a two-seat German trainer aircraft of the 1920s. It was a single-engine biplane of conventional configuration that seated the pilot and instructor in tandem, open cockpits. The wings were of unequal span and had a pronounced stagger.
Variants
Specifications (L 68c)
General characteristics
- Crew: two, pilot and instructor
- Length: 6.30 m (20 ft 8 in)
- Wingspan: 10.10 m (33 ft 2 in)
- Height: 2.56 m (8 ft 5 in)
- Wing area: 24.4 m2 (263 ft2)
- Empty weight: 650 kg (1,430 lb)
- Gross weight: 950 kg (2,090 lb)
- Powerplant: 1 × Siemens-Halske Sh 12, 80 kW (110 hp)
Performance
- Maximum speed: 140 km/h (90 mph)
- Range: 360 km (220 miles)
- Service ceiling: 4,200 m (13,800 ft)
- Rate of climb: 1.4 m/s (270 ft/min)
See also
References
|
---|
| Pre World War I aircraft | |
---|
| German military aircraft of World War I | |
---|
| Post wartype company designations |
- L.3
- L.9
- L.58
- L.59
- L.60
- L.65
- L.66
- L.67
- L.68
- L.69
- L.70
- L.71
- L.72
- L.72A
- L.73
- L.74
- L.75
- L.76
- L.77
- L.78
- L.79
- L.81
- L.82
- L.83
- L.84
- L.101
- L.102
- L.103
|
---|
|
|
---|
| General | |
---|
| Military | |
---|
| Accidents / incidents | |
---|
| Records | |
---|
| Misc. | |
---|
|