fbpx
Wikipedia

Coser-Oonk CO-2

The Coser-Oonk CO-2 "Our Lady" is a single-place, open-cockpit, low-winged monoplane homebuilt aircraft design.[1]

Coser-Oonk CO-2
Role Homebuilt aircraft
National origin United States
Designer Joseoh Coser, Jack Oonk
First flight 15 September 1959

Design and development

The CO-2 was originally started as a mid-wing, but was changed to a low-wing for improved visibility.[2]

The CO-2 is a single-place, strut-braced, low-wing conventional geared monoplane. The tail section is modified from a Luscombe fuselage. The wings were also sourced from a Luscombe, but strut braced from the top and shortened.

Operational history

Test flights were performed at Creve Coeur Airport in 1959.

Specifications (Coser-Oonk CO-2)

Data from Sport Aviation

General characteristics

  • Capacity: 1
  • Length: 18 ft 5 in (5.61 m)
  • Wingspan: 19 ft 6 in (5.94 m)
  • Wing area: 81 sq ft (7.5 m2)
  • Empty weight: 690 lb (313 kg)
  • Gross weight: 1,050 lb (476 kg)
  • Fuel capacity: 14 US gallons (53 l; 12 imp gal)
  • Powerplant: 1 × Continental A75 , 75 hp (56 kW)

Performance

  • Cruise speed: 109 kn (125 mph, 201 km/h)
  • Stall speed: 52 kn (60 mph, 97 km/h)

See also

  • Image of the CO-2 [1]

Aircraft of comparable role, configuration, and era

References

  1. ^ Bill Gunston (1993). World encyclopaedia of aircraft manufacturers: from the pioneers to the present day. ISBN 9781557509390.
  2. ^ Sport Aviation. September 1960. {{cite journal}}: Missing or empty |title= (help)

coser, oonk, lady, single, place, open, cockpit, winged, monoplane, homebuilt, aircraft, design, role, homebuilt, aircraftnational, origin, united, statesdesigner, joseoh, coser, jack, oonkfirst, flight, september, 1959, contents, design, development, operatio. The Coser Oonk CO 2 Our Lady is a single place open cockpit low winged monoplane homebuilt aircraft design 1 Coser Oonk CO 2Role Homebuilt aircraftNational origin United StatesDesigner Joseoh Coser Jack OonkFirst flight 15 September 1959 Contents 1 Design and development 2 Operational history 3 Specifications Coser Oonk CO 2 4 See also 5 ReferencesDesign and development EditThe CO 2 was originally started as a mid wing but was changed to a low wing for improved visibility 2 The CO 2 is a single place strut braced low wing conventional geared monoplane The tail section is modified from a Luscombe fuselage The wings were also sourced from a Luscombe but strut braced from the top and shortened Operational history EditTest flights were performed at Creve Coeur Airport in 1959 Specifications Coser Oonk CO 2 EditData from Sport AviationGeneral characteristicsCapacity 1 Length 18 ft 5 in 5 61 m Wingspan 19 ft 6 in 5 94 m Wing area 81 sq ft 7 5 m2 Empty weight 690 lb 313 kg Gross weight 1 050 lb 476 kg Fuel capacity 14 US gallons 53 l 12 imp gal Powerplant 1 Continental A75 75 hp 56 kW Performance Cruise speed 109 kn 125 mph 201 km h Stall speed 52 kn 60 mph 97 km h See also EditImage of the CO 2 1 Aircraft of comparable role configuration and era Stits Playboy Poberezny P 5 Pober SportReferences Edit Bill Gunston 1993 World encyclopaedia of aircraft manufacturers from the pioneers to the present day ISBN 9781557509390 Sport Aviation September 1960 a href Template Cite journal html title Template Cite journal cite journal a Missing or empty title help Retrieved from https en wikipedia org w index php title Coser Oonk CO 2 amp oldid 1104276621, wikipedia, wiki, book, books, library,

article

, read, download, free, free download, mp3, video, mp4, 3gp, jpg, jpeg, gif, png, picture, music, song, movie, book, game, games.