Gallaudet D-4

Gallaudet D-4
General information
Type	Observation aircraft
Manufacturer	Gallaudet Aircraft Company
Primary user	United States Navy
Number built	2
History
Introduction date	1918
First flight	1918

The Gallaudet D-4 was an unusual biplane designed and built by Gallaudet Aircraft Company for the United States Navy. It was powered by a Liberty L-12 engine buried within the fuselage which turned a large, four-bladed propeller attached to a ring around the center fuselage. Only two were constructed, with the second being accepted by the Navy for service as an observation aircraft. ^[1]

Development

In response to a requirement by the U.S. Navy for light floatplanes capable of being launched off catapults by ships underway, the Gallaudet Aircraft company began development of the "D-4", based on the earlier Gallaudet D-1. The D-1 was powered by two Duesenberg engines of 150 hp (110 kW) each and used a clutch mechanism to allow the use of one or both engines. ^[2]

Operational history

Two D-4s were built, serial numbers A:2653 and A:2654. The prototype crashed as result of a failed elevator control during flight testing on 19 July 1918, killing the pilot, Lt. Arthur Souther. The second D4 first flew in October 1918 and was accepted by the U.S. Navy in April 1919. This aircraft was entered in the Curtiss Marine Trophy Race during the National Air Races in Detroit Michigan on October 8, 1922, but had to leave the race after the fifth lap because of a broken propeller. ^[3]

Operators

  United States

• United States Navy

Specifications

Data fromAmerican Combat Planes, p. 118 ^[1]

General characteristics

• Crew: two (pilot, observer)
• Length: 33 ft 6 in (10.2 m)
• Wingspan: 46 ft 5 in (14.1 m)
• Height: 11 ft 8 in (3.6 m)
• Wing area: 612 sq ft (56.9 m²)
• Empty weight: 4,228 lb (1,918 kg)
• Gross weight: 5,440 lb (2,468 kg)
• Powerplant: 1 × Liberty L-12 V-12 water-cooled piston engine , 360 hp (269 kW)

Performance

• Maximum speed: 119 mph (192 km/h, 103 kn) landing speed 58 mph
• Range: 390 mi (628 km, 340 nmi)
• Endurance: 3 hours 30 minutes
• Service ceiling: 14,000 ft (4,267 m)

Armament

• None

See also

Related development

• Gallaudet D-1
• Gallaudet D-2

Aircraft of comparable role, configuration, and era

• Curtiss R-6
• Royal Aircraft Factory B.E.9
• SPAD S.A

References

1. Wagner, Ray (1982). American Combat Planes, Third Edition . USA: Doubleday & Company. ISBN   0-385-13120-8.
2. "Gallaudet D-1 / D-4". flyingmachines.ru. Retrieved 31 October 2015.
3. Robert Gordon. "GALLAUDET D-1". earlyaviators.com. Archived from the original on 7 February 2007. Retrieved 31 October 2015.

Bibliography

• Casari, Robert B. (2014). American MIlitary Aircraft 1908–1919. n.p.: Aeronaut Books. ISBN   978-1-935881-13-1.
• "The Gallaudet Story: Part 16A: The Model D-4". WWI Aero: The Journal of the Early Aeroplane (196): 28–46. May 2007. ISSN   0736-198X.
• "The Gallaudet Story: Part 16B: The Model D-4 Continued". WWI Aero: The Journal of the Early Aeroplane (197): 28–49. August 2007. ISSN   0736-198X.

External links

• Photos of D-4 at airminded.net. Accessed 2011-09-30.
• Photo of D-4 at earlyaviators.com. Accessed 2011-09-30.