Trek Aerospace Dragonfly
From Wikipedia, the free encyclopedia
The Trek Aerospace Dragonfly is a horizontally configured cargo-carrying aircraft from Trek Aerospace that began development in 2004. The Dragonfly has the ability to quickly change its flight options from remote, to unmanned, or manned.[citation needed] With the additional ability to transport a payload, utilizing a minimal takeoff space, the Dragonfly is an up-and-coming frontrunner in the VTOL and PAV market.
Specifications (Dragonfly UMR-1)
General characteristics
- Crew: one, pilot (or remotely piloted)
- Capacity: 41.2 ft³ (1.67 m³), 450 lb (204 kg) payload
- Length: 13.1 ft (4.0 m)
- Width (duct assembly): 9.7 ft (3.0 m)
- Wing area: ft² ( m²)
- Empty: 490 lb (222 kg)
- Loaded: 810 lb (367 kg)
- Maximum takeoff: 1,070 lb (485 kg)
- Powerplant: 1× rotary engine, 177 hp (132 kW)
Performance
- Maximum speed: 235 mph (378 km/h)
- Range: over 575 miles (over 925 km)
- Service ceiling: 12,900 ft (3,900 m)
- Rate of climb: 5,500 ft/min (1,676 m/min)
- Wing loading: kg/m² ( lb/ft²)
- Power/mass: hp/lb ( kW/kg)
External links
|
This article is issued from Wikipedia. The text is available under the Creative Commons Attribution/Share Alike; additional terms may apply for the media files.