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Douglas Cloudster II

General Aviation and Light Aircraft

The Douglas Cloudster II was an American prototype five-seat light aircraft of the late 1940s with an unusual layout: two air-cooled piston engines buried in the rear fuselage drove a single eight-foot twin-bladed pusher propeller mounted behind the tail through driveshafts taken from P-39 fighters. Douglas had developed this buried-engine configuration in the early 1940s to cut drag and first demonstrated it in the XB-42 Mixmaster, then applied it to the Model 1015 Cloudster II for executive or air charter use. The pilot and four passengers sat in an enclosed cabin ahead of the unswept laminar flow wing. It made its maiden flight on March 12, 1947 and had good performance and handling, but it suffered excessive vibration and overheated on the ground; development was abandoned late in 1947 after only two flights, as the selling price had risen from a planned 30,000 dollars to 68,000.

Facts
Year
1947 1
Engine Class
Piston 1
Status
Abandoned 1
Mass (kg)
1451 1
Maximum Mass (kg)
2307 1
Comparison
Body Style
Aircraft (no road body style) 1
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Exemplifies

Aviation, Modes
Source Douglas Cloudster II (Wikipedia)

Of Make

Source Douglas Cloudster II (Wikipedia)
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Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Douglas Cloudster II (Wikipedia)Lead, manufacturer
Quote, Lead, manufacturer
Douglas Aircraft Company developed a configuration for high-performance twin-engined aircraft

Originated In

Also in Geography Atlas: where this subject originated.

Source Douglas Cloudster II (Wikipedia)Lead, country of origin
Quote, Lead, country of origin
The Douglas Cloudster II was an American prototype five-seat light aircraft of the late 1940s
Sources
1. Douglas Cloudster II (Wikipedia)
  • Design and development
    The Cloudster II made its maiden flight on March 12, 1947
  • Lead
    prototype five-seat light aircraft
  • Specifications
    Continental E250 six-cylinder air-cooled piston engine
  • Design and development, status
    Further development was abandoned late in 1947
  • Specifications, mass
    Empty weight: 3,200 lb (1,451 kg)
  • Specifications, maximum mass
    Gross weight: 5,085 lb (2,307 kg)
  • Lead, manufacturer
    Douglas Aircraft Company developed a configuration for high-performance twin-engined aircraft
  • Lead, country of origin
    The Douglas Cloudster II was an American prototype five-seat light aircraft of the late 1940s
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