Douglas Cloudster

The Davis-Douglas Company was formed in July 1920 to enable Donald Douglas to design and build an aircraft capable of non-stop flight coast-to-coast across the United States. David R. Davis provided the financing for the company. The resulting aircraft was the Cloudster, a single-bay equal-span biplane of wooden construction. It was fabric-covered except for the forward fuselage, which was covered with sheet metal. The aircraft was powered by a 400 hp (298 kW) Liberty V-12 piston engine.

The Cloudster first flew on 24 February 1921 and attempted the coast-to-coast journey in June that year. The aircraft failed to make a non-stop journey due to engine failure. In 1923, the Cloudster was sold and modified for sightseeing flights, with two additional open cockpits and seats for five passengers replacing one of the fuel tanks. In 1925 it was again sold to T. Claude Ryan, who had it modified further by adding an enclosed cabin with ten seats.[1][2] It was subsequently used by a number of operators before it made a forced landing in shallow water off the coast of Ensenada, Baja California in December 1926. It was damaged beyond repair by the tide before it could be recovered.

Following the failure of the coast-to-coast flight, Davis lost interest and Douglas went on to form the Douglas Company (later the Douglas Aircraft Company) in July 1921.

Douglas Aircraft would revive the name in 1945 for a proposed general aviation aircraft with a pusher propellor, similar to the XB-42, as the Cloudster II.[3][4][5][6] The company's last effort in general aviation, it was not a success.[3][7]

Data from McDonnell Douglas aircraft since 1920 : Volume I[2]

General characteristics

• Length: 36 ft 9 in (11.20 m)
• Wingspan: 55 ft 11 in (17.04 m)
• Height: 12 ft 0 in (3.66 m)
• Gross weight: 9,600 lb (4,354 kg)
• Fuel capacity: 660 US gal (550 imp gal; 2,500 l) fuel in two fuel tanks with 50 US gal (42 imp gal; 190 l) oil in a single tank
• Powerplant: 1 × Liberty L-12 V-12 water-cooled piston engine, 400 hp (300 kW)
• Propellers: 2-bladed fixed-pitch wooden propeller

Performance

• Maximum speed: 120 mph (190 km/h, 100 kn)
• Cruise speed: 85 mph (137 km/h, 74 kn)
• Range: 550 mi (890 km, 480 nmi)
• Ferry range: 2,800 mi (4,500 km, 2,400 nmi)
• Endurance: 33 hours
• Service ceiling: 19,160 ft (5,840 m)
• Power/mass: 0.417 hp/lb (0.686 kW/kg)

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Notes

Bibliography

• The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985), 1985, Orbis Publishing
• Francillon, René J. (1979). McDonnell Douglas Aircraft since 1920. London: Putnam. ISBN 0-370-00050-1.
• Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions.