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Team Rocket F1 Rocket

The Team Rocket F1 Rocket is a two-seat sport plane formerly built in Czech Republic and marketed as a kit for amateur construction by Team Rocket of Texas, United States. As of April 2017, the aircraft is being produced in the U.S. under license from Team Rocket by Frazier Aviation Products LLC of Indiana.

F1 Evo
Role Sport monoplane
National origin United States
Designer Team Rocket
First flight 2000
Number built 130+

Development and design

The F1 Rocket is a tandem two-seat low-wing cantilever monoplane built mainly in aluminum.[1] The Rocket has a titanium 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] Tip up canopies are also used. The prototype first flew in the United States in November 2000 and by 2003 seven others had flown. By late 2017, over 130 had flown.[2]

Variants

F1 Rocket
Tandem-seat variant using a 6 cylinder Lycoming IO-540 or Continental IO-550 engine of 250-350 HP. The wing on the F1 is similar to the Vans RV-4 wing, a rectangular design with slotted ailerons, and bottom hinged flaps. The canopy may be a slider or flip over design, but most use the slider design.[2]
 
F1 Evo
F1 Evo
Evolutionary variant design, utilized a tapered wing as compared to the rectangular wing on the F1. Significant changes were made to the aileron and flap design. F1 Evo uses the same fuselage and tail as the original F1. The Evo wing is no longer available.
 
F4 in flight
F4 Raider
Tandem-seat variant using a 4-cylinder Lycoming or clone.[2]

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 (407 km/h, 220 kn)
  • Cruise speed: 230 mph (370 km/h, 200 kn) 75% Power
  • Stall speed: 54 mph (87 km/h, 47 kn)
  • Range: 1,150 mi (1,850 km, 1,000 nmi) 55% Power
  • Rate of climb: 3,500 ft/min (18 m/s)

References

Notes

  1. ^ a b c d Jackson 2003, p. 740
  2. ^ a b c "Home of the F1 Rocket and F4 Raider - Team Rocket". Team Rocket. Retrieved 2018-05-05.

Bibliography

  • Jackson, Paul, ed. (2003). Jane's All the World's Aircraft 2003-04. Coulsdon, Surrey, United Kingdom: Jane's Information Group. ISBN 0-7106-2537-5.

team, rocket, rocket, seat, sport, plane, formerly, built, czech, republic, marketed, amateur, construction, team, rocket, texas, united, states, april, 2017, aircraft, being, produced, under, license, from, team, rocket, frazier, aviation, products, indiana, . The Team Rocket F1 Rocket is a two seat sport plane formerly built in Czech Republic and marketed as a kit for amateur construction by Team Rocket of Texas United States As of April 2017 the aircraft is being produced in the U S under license from Team Rocket by Frazier Aviation Products LLC of Indiana F1 EvoRole Sport monoplaneNational origin United StatesDesigner Team RocketFirst flight 2000Number built 130 Contents 1 Development and design 2 Variants 3 Specifications F1 Rocket 4 References 4 1 Notes 4 2 BibliographyDevelopment and design EditThe F1 Rocket is a tandem two seat low wing cantilever monoplane built mainly in aluminum 1 The Rocket has a titanium 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 Tip up canopies are also used The prototype first flew in the United States in November 2000 and by 2003 seven others had flown By late 2017 over 130 had flown 2 Variants EditF1 Rocket Tandem seat variant using a 6 cylinder Lycoming IO 540 or Continental IO 550 engine of 250 350 HP The wing on the F1 is similar to the Vans RV 4 wing a rectangular design with slotted ailerons and bottom hinged flaps The canopy may be a slider or flip over design but most use the slider design 2 F1 EvoF1 Evo Evolutionary variant design utilized a tapered wing as compared to the rectangular wing on the F1 Significant changes were made to the aileron and flap design F1 Evo uses the same fuselage and tail as the original F1 The Evo wing is no longer available F4 in flightF4 Raider Tandem seat variant using a 4 cylinder Lycoming or clone 2 Specifications F1 Rocket EditData from Jane s All the World s Aircraft 2003 04 1 General characteristicsCrew 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 bladedPerformance Maximum speed 253 mph 407 km h 220 kn Cruise speed 230 mph 370 km h 200 kn 75 Power Stall speed 54 mph 87 km h 47 kn Range 1 150 mi 1 850 km 1 000 nmi 55 Power Rate of climb 3 500 ft min 18 m s References EditNotes Edit a b c d Jackson 2003 p 740 a b c Home of the F1 Rocket and F4 Raider Team Rocket Team Rocket Retrieved 2018 05 05 Bibliography Edit Wikimedia Commons has media related to Team Rocket F1 Rocket Jackson Paul ed 2003 Jane s All the World s Aircraft 2003 04 Coulsdon Surrey United Kingdom Jane s Information Group ISBN 0 7106 2537 5 Retrieved from https en wikipedia org w index php title Team Rocket F1 Rocket amp oldid 1147144080, wikipedia, wiki, book, books, library,

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