| Sablatnig C.I | |
|---|---|
.jpg.webp) | |
| Role | Reconnaissance two-seater |
| National origin | Germany |
| Manufacturer | Sablatnig |
| Produced | 1917 |
| Number built | ~2 |
The Sablatnig C.I was a conventional C-type reconnaissance two-seater aircraft developed and built by Sablatnig in Berlin, Germany in 1917. It was a two-bay biplane of conventional design, with staggered wings, two open cockpits in tandem, and fixed, tailskid undercarriage.
The C.I was developed into the Sablatnig N.I in 1918.
Specifications
General characteristics
- Length: 8.7 m (28 ft 7 in)
- Wingspan: 16.0 m (52 ft 6 in)
- Empty weight: 1,050 kg (2,315 lb)
- Gross weight: 1,540 kg (3,395 lb)
- Powerplant: 1 × Argus As III , 130 kW (180 hp)
- Propellers: 2-bladed
Performance
- Maximum speed: 120 km/h (75 mph, 65 kn)
- Time to altitude: 9 min to 3,281 ft (1,000 m)
Armament
- Guns: 1 x Parabellum machine-gun
- Bombs: 6 x 110 lb (50 kg) bombs
Notes
References
External links
Wikimedia Commons has media related to Sablatnig C.I.
This article is issued from Wikipedia. The text is licensed under Creative Commons - Attribution - Sharealike. Additional terms may apply for the media files.