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Pope Thunderbird P-2

The Pope Thunderbird is an American homebuilt biplane designed by Leon Pope.

Pope Thunderbird P-2
Role Homebuilt aircraft
National origin United States
Designer Leon Pope

Design and development edit

The Pope Thunderbird P-2 is a single engine, conventional landing gear-equipped, open cockpit biplane.[1][2] The aircraft was designed by Leon Pope of Plymouth, Michigan and made its maiden flight on June 18, 1959.[3]

Specifications edit

Data from Jane's All The World's Aircraft 1961–62[3]

General characteristics

  • Crew: 1
  • Length: 15 ft 0 in (4.57 m)
  • Wingspan: 18 ft 3 in (5.56 m)
  • Height: 5 ft 9 in (1.75 m)
  • Wing area: 120 sq ft (11 m2)
  • Aspect ratio: 5.7:1
  • Airfoil: S-1A
  • Empty weight: 800 lb (363 kg)
  • Gross weight: 1,080 lb (490 kg)
  • Powerplant: 1 × Lycoming O-235-C four-cylinder horizontally opposed piston aircraft engine, 100 hp (75 kW)

Performance

  • Maximum speed: 135 mph (217 km/h, 117 kn)
  • Cruise speed: 115 mph (185 km/h, 100 kn)
  • Stall speed: 55 mph (89 km/h, 48 kn)312 h
  • Rate of climb: 1,000 ft/min (5.1 m/s)

References edit

  1. ^ "Experimental Aircraft Fly-In". Flying. Vol. 67, no. 5. November 1960. pp. 36–37.
  2. ^ Kohn, Leo J (December 1961). "EAA Fly-in". Flying. Vol. 69, no. 6. pp. 34–35.
  3. ^ a b Taylor 1961, p. 309.
  • Taylor, John W. R. (1961). Jane's All The World's Aircraft 1961–62. London: Sampson Low, Marston & Company, Ltd.

pope, thunderbird, pope, thunderbird, american, homebuilt, biplane, designed, leon, pope, role, homebuilt, aircraftnational, origin, united, statesdesigner, leon, popedesign, development, editthe, single, engine, conventional, landing, gear, equipped, open, co. The Pope Thunderbird is an American homebuilt biplane designed by Leon Pope Pope Thunderbird P 2Role Homebuilt aircraftNational origin United StatesDesigner Leon PopeDesign and development editThe Pope Thunderbird P 2 is a single engine conventional landing gear equipped open cockpit biplane 1 2 The aircraft was designed by Leon Pope of Plymouth Michigan and made its maiden flight on June 18 1959 3 Specifications editData from Jane s All The World s Aircraft 1961 62 3 General characteristicsCrew 1 Length 15 ft 0 in 4 57 m Wingspan 18 ft 3 in 5 56 m Height 5 ft 9 in 1 75 m Wing area 120 sq ft 11 m2 Aspect ratio 5 7 1 Airfoil S 1A Empty weight 800 lb 363 kg Gross weight 1 080 lb 490 kg Powerplant 1 Lycoming O 235 C four cylinder horizontally opposed piston aircraft engine 100 hp 75 kW Performance Maximum speed 135 mph 217 km h 117 kn Cruise speed 115 mph 185 km h 100 kn Stall speed 55 mph 89 km h 48 kn 31 2 h Rate of climb 1 000 ft min 5 1 m s References edit Experimental Aircraft Fly In Flying Vol 67 no 5 November 1960 pp 36 37 Kohn Leo J December 1961 EAA Fly in Flying Vol 69 no 6 pp 34 35 a b Taylor 1961 p 309 Taylor John W R 1961 Jane s All The World s Aircraft 1961 62 London Sampson Low Marston amp Company Ltd Retrieved from https en wikipedia org w index php title Pope Thunderbird P 2 amp oldid 1066540281, wikipedia, wiki, book, books, library,

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