Engineering:Caspar C 33
From HandWiki
| C 33 | |
|---|---|
| Role | Training aircraft |
| Manufacturer | Caspar-Werke |
| Designer | Reinhold Mewes |
| First flight | 1928 |
| Number built | 1 |
The Caspar C 33 was a training aircraft developed in Germany in the late 1920s.
Specifications
Data from [1]
General characteristics
- Crew: 2
- Length: 5.30 m (17 ft 5 in)
- Wingspan: 8.00 m (26 ft 3 in)
- Empty weight: 490 kg (1,080 lb)
- Gross weight: 750 kg (1,653 lb)
- Powerplant: 1 × Armstrong-Siddeley Mongoose 5-cylinder air-cooled radial piston engine, 101 kW (135 hp)
- Propellers: 2-bladed fixed pitch propeller
Performance
- Maximum speed: 160 km/h (99 mph, 86 kn)
- Cruise speed: 130 km/h (81 mph, 70 kn)
References
- ↑ "Caspar C 33" (in Russian). Moscow. http://www.airwar.ru/enc/other1/casparc33.html. Retrieved 26 February 2019.
 |  |
