Nicholson Junior KN-2
The Nicholson Junior KN-2 was an aircraft made in the late 1920s. It was used for flight training in the United States. Only 1 aircraft was built.
Specifications
General characteristics
- Crew: one
- Capacity: one passenger or student
- Length: 23 ft (7.0 m)
- Wingspan: 37 ft (11 m)
- Wing area: 190 sq ft (18 m2) plus 21.5 sq ft (2.00 m2) ailerons
- Empty weight: 540 lb (245 kg)
- Fuel capacity: 11 US gal (9.2 imp gal; 42 l)
- Engine: 1 × Continental A40 flat four or Szekely SR-3 3 cylinder radial engine
- Propellers: 2-bladed
Performance
- Maximum speed: 85 mph (137 km/h, 74 kn)
- Cruise speed: 75 mph (121 km/h, 65 kn)
- Landing speed: 28 mph (45 km/h; 24 kn)
- Take-off time: 8 s
- Range: 315 mi (507 km, 274 nmi)
- Service ceiling: 10,000 ft (3,000 m)