Team Rocket F1 Rocket
F1 Rocket | |
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Role | Sport monoplane |
National origin | United States |
Designer | International High Performance Aircraft |
First flight | 2000 |
Number built | 7+ |
Developed from | Van's Aircraft RV-4 |
The Team Rocket F1 Rocket is a two-seat sportplane designed in Czech Republic by International High Performance Aircraft and marketed as a kit for amateur construction by Team Rocket of Texas, United States.
Development and design
The F1 Rocket is a tandem two-seat low-wing cantilever monoplane built mainly in Aluminium.[1] The Rocket has a fixed conventional landing gear with a tailwheel. Designed to be built with a range of nose-mounted engines between 235 and 350 hp (175 and 224 kW) the prototype has a Lycoming IO-540 with a three-bladed propeller.[1] The F1 has tandem seating for two with a rear-sliding canopy and a fixed windscreen.[1] The prototype first flew in the United States in November 2000 and by 2003 seven others had flown. By 2014, over 80 had flown.[2]
Variants
- F1 Rocket
- Tandem-seat variant
- F1 Evo
- Evolutionary variant design, powered by a 350 hp (261 kW) Continental IO-550, giving a cruise speed of 240 mph (386 km/h) and a rate of climb of 3445 fpm (17.5 m/s).[3]
Specifications (F1 Rocket)
Data from Jane's All the World's Aircraft 2003-04[1]
General characteristics
- Crew: 2
- Length: 21 ft 0 in (6.40 m)
- Wingspan: 21 ft 6 in (6.56 m)
- Wing area: 106.0 sq ft (9.85 m2)
- Empty weight: 1,199 lb (544 kg)
- Max takeoff weight: 2,000 lb (907 kg)
- Powerplant: 1 × Lycoming IO-540 Flat-six piston engine, 260 hp (190 kW)
- Propellers: 3-bladed
Performance
- Maximum speed: 253 mph; 220 kn (407 km/h)
- Cruising speed: 230 mph; 200 kn (370 km/h) 75% Power
- Stall speed: 54 mph; 47 kn (87 km/h)
- Range: 1,150 mi; 999 nmi (1,850 km) 55% Power
- Rate of climb: 3,500 ft/min (18 m/s)
References
Notes
Bibliography
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Wikimedia Commons has media related to Team Rocket F1 Rocket. |
- Jackson, ed. (2003). Jane's All the World's Aircraft 2003-04. Coulsdon, Surrey, United Kingdom: Jane's Information Group. ISBN 0-7106-2537-5.
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