Pop's Props Cloudster
The Pop's Props Cloudster is a single seat, open-cockpit, parasol wing, single-engine monoplane, that was first flown in 1995. The aircraft was produced by Pop's Props of Cooksville, Illinois and made available as plans or in kit form. The company is no longer in business and kit production has been transferred to Simplex Aeroplanes of Old Saybrook, Connecticut. The aircraft was designed for the FAR 103 Ultralight Vehicles category, including the category's 254 lb (115 kg) empty weight limit. The standard empty weight of the Cloudster is 250 lb (113 kg).
Summary from Wikipedia licensed under CC BY-SA.
- Manufacturer
- Pop's Props
- Country of origin
- United States
- First flight
- 1995-01-01
Specifications
- Cruise speed
- 43 kt
- Max speed
- 52 kt
- Range
- 75 nm
- Service ceiling
- 6,000 ft
- Rate of climb
- 650 ft/min
- Max takeoff weight
- 500 lb
- Empty weight
- 250 lb
- Fuel capacity
- 2.5 US gal
- Powerplant
- Kawasaki 340-LC
- Engines
- 1
- Seats
- 1
- Length
- 16.5 ft
- Wingspan
- 30 ft
- Height
- 7 ft
- Number built
- 3
Specifications are approximate and may vary by variant. Compiled from Wikipedia (CC BY-SA).
Reference and training only. Specifications vary by variant — consult the manufacturer and the official documents.