Team Rocket F1 Rocket

F1 Rocket
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

Performance


References

Notes

  1. 1 2 3 4 Jackson 2003, p. 740
  2. Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 123. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X

Bibliography

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.  |first1= missing |last1= in Authors list (help)
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