D-1 | |
---|---|
D-1 at Naval Air Station Pensacola, Florida, 16 January 1916 | |
Role | Observation aircraft |
Manufacturer | Gallaudet Aircraft Company |
Designer | Edson Gallaudet |
First flight | 17 July 1916 |
Number built | 1 prototype |
Developed into | Gallaudet D-2 |
The Gallaudet D-1 was a prototype American biplane observation aircraft built by the Gallaudet Aircraft Company during World War I for the United States Navy. The aircraft was completed in 1916.
Background and description
The D-1 was designed to partially meet an requirement for a two-seat, twin-float, twin-engined biplane for maritime-patrol duties issued by the United States Navy in February 1915. Edson Gallaudet, chief designer for the Gallaudet Aircraft Company, had submitted a design using his revolutionary "Gallaudet Drive" in which the propeller revolved around a hub buried in the middle of the fuselage.[1]
Specifications (D-2)
Data from The Gallaudet Story: Part 8B: The D-1 Hydroplane for the Army;[2] American Military Aircraft, 1908–1919[3]
General characteristics
- Crew: 2
- Length: 33 ft (10 m)
- Upper wingspan: 48 ft (15 m)
- Height: 13 ft (4.0 m)
- Wing area: 658 sq ft (61.1 m2)
- Empty weight: 3,600 lb (1,633 kg)
- Gross weight: 4,604 lb (2,088 kg)
- Powerplant: 2 × Duesenberg water-cooled, straight 4 piston engine, 150 hp (110 kW) each
- Propellers: 4-bladed fixed-pitch propeller, 9 ft 6 in (2.90 m) diameter
Performance
- Maximum speed: 91 mph (146 km/h, 79 kn)
- Endurance: 4 hours (at full speed)
- Time to altitude: 5 minutes to 900 ft (270 m)
References
Bibliography
- Casari, Robert B. (2014). American MIlitary Aircraft 1908–1919. n.p.: Aeronaut Boooks. ISBN 978-1-935881-13-1.
- Gordon, Robert (August 2004). "The Gallaudet Story: Part 8A: The D-1 Hydroplane for the Navy". WWI Aero: The Journal of the Early Aeroplane (185): 30–45. ISSN 0736-198X.
- Gordon, Robert (November 2004). "The Gallaudet Story: Part 8B: The D-1 Hydroplane for the Navy". WWI Aero: The Journal of the Early Aeroplane (186): 12–21. ISSN 0736-198X.
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