Today In Aviation History: First Flight of the Douglas Cloudster II

The Douglas Cloudster II first flew on March 12, 1947, as an experimental executive aircraft built around an unconventional propulsion layout. Two engines mounted inside the fuselage drove a single pusher propeller at the rear, a concept inspired by Douglas’ earlier XB-42 Mixmaster bomber. Although the prototype showed promising speed and handling, vibration issues, overheating, and rising costs led to the project’s cancellation after only two flights.

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Austin Hancock
Photo via Douglas Aircraft Company
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On this day in aviation history, 79 years ago (March 12, 1947), the first flight of the Douglas Cloudster II took place. An unusual design, the Cloudster II was a prototype low-wing, twin-engine light aircraft. Douglas developed this aircraft with an unconventional layout. The engines were placed inside the fuselage, and they drove a single pusher propeller at the rear of the aircraft. The Cloudster II was a furtherance of Douglas Aircraft’s earlier 1940s designs, such as the XB-42 Mixmaster prototype bomber. Douglas was experimenting to reduce the overall drag of their multi-engined aircraft. They believed that by eliminating engines protruding from the wings and integrating them into the fuselage instead, drag would be greatly reduced. Their theory was proven correct by the XB-42, which saw a 30% decrease in drag, compared to conventional multi-engine aircraft, during flight testing. Additionally, the Mixmaster showed improved handling with an engine out, meaning asymmetric thrust had also been reduced.

Douglas Cloudster II
Douglas Cloudster II. Photo via Wikipedia

Douglas Aircraft hoped to carry over the success of the XB-42’s flight characteristics into a new medium-range airliner design, the DC-8. In parallel to the DC-8 prototype, Douglas also began development of the Model 1015, Cloudster II, as an executive aircraft. The Cloudster II had a single pilot and a capacity for four passengers. Douglas opted for an unswept laminar-flow wing in their design. The twin 250-horsepower Continental E250 6-cylinder engines were installed in the rear fuselage, driving a single 8-foot-diameter twin-bladed propeller. This prop was mounted aft of the empennage and connected to the E250s via driveshafts, which were taken from the Bell P-39 Airacobra.

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Photo via Douglas Aircraft Company

The Cloudster II had good performance and handling during initial flight testing. The aircraft could cruise at 200 mph and attain a maximum airspeed of 229 mph. A range of 830 nautical miles, a service ceiling of 22,200 feet, and a 1,500 feet per minute rate of climb made the Cloudster II a competitive executive aircraft design. As flight testing progressed, the aircraft was found to suffer from excessive vibration and was also prone to overheating on the ground. The sole prototype only flew twice, and the Cloudster II was abandoned in late 1947. The aircraft’s performance aside, the civilian aircraft market had not proven as fruitful as hoped. An originally planned selling price of $30,000 USD had jumped to $68,000, thus making the Cloudster II an impractical option.

Douglas Cloudster II Front Quarter Douglas Aircraft Company
Photo via Douglas Aircraft Company
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Commercial Pilot, CFI, and Museum Entrepreneur, with a subject focus on WWII Aviation. I am dedicated to building flight experience so I can fly WWII Fighters, such as the P-51 Mustang, for museums and airshows, and in the USAF Heritage Flight. I lead and run the Pennington Flight Memorial, to honor local MIA Tuskegee Airman F/O Leland “Sticky” Pennington.
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