Kaminskas Jungster II
| Jungster II | |
|---|---|
| Role | Homebuilt aircraft |
| National origin | United States |
| Designer | Rim Kaminskas |
| First flight | March 1966[1] |
| Developed from | Kaminskas Jungster I |
The Jungster II is a parasol wing homebuilt aircraft. Designed by Rim Kaminskas, it first flew in March 1966.[2]
Design and development
The Jungster II is a parasol version based on the previous Jungster I biplane design, which itself was a scaled down version of the Bücker Bü 133 biplane. Plans were distributed by K&S aircraft supply.
The aircraft is a single-seat, open cockpit, strut-braced, parasol wing design with conventional landing gear. The airframe can accommodate engines ranging from 85 to 180 hp (63 to 134 kW). The fuselage is constructed of welded steel tubing with aircraft fabric covering. The wing has a slight rearward sweep.[3]
Specifications (Jungster II)
Data from Plane & Pilot
General characteristics
- Length: 16 ft 11 in (5.16 m)
- Wingspan: 22 ft 4 in (6.81 m)
- Wing area: 80 sq ft (7.4 m2)
- Airfoil: NACA 2412
- Empty weight: 739 lb (335 kg)
- Gross weight: 1,375 lb (624 kg)
- Fuel capacity: 16 U.S. gallons (61 L; 13 imp gal)
- Propellers: 2-bladed
Performance
- Maximum speed: 148 kn; 274 km/h (170 mph)
- Cruise speed: 129 kn; 238 km/h (148 mph)
- Rate of climb: 3,500 ft/min (18 m/s)
See also
- Aircraft of comparable role, configuration and era
References
- ↑ Bill Gunston. World encyclopaedia of aircraft manufacturers: from the pioneers to the present day.
- ↑ Air Trails: 76. Winter 1971. Missing or empty
|title=(help) - ↑ "Jungster II". Retrieved 9 February 2012.
External links
This article is issued from Wikipedia - version of the 6/24/2015. The text is available under the Creative Commons Attribution/Share Alike but additional terms may apply for the media files.