Dornier Do 10

Do 10
General information
Type	Fighter aircraft
National origin	Germany
Manufacturer	Dornier Flugzeugwerke
History
First flight	24 July 1931
Developed from	Dornier Komet

The Dornier Do 10, originally designated Dornier Do C4, was the name given by the Reichsluftfahrtministerium (RLM) of a pre-World War II German aircraft.

It was a two-seat parasol-wing monoplane, intended to be used as a fighter. Two prototypes were built in 1931 to fulfil a requirement for a two-seat fighter. Having failed to gain a production order, the Do C4 / Do 10 was used to test a tilting engine installation and propellers to suit, for STOL tests.

Specifications

Dornier Do C4 3-view drawing from L'Aerophile July 1934

Type	Two-seat fighter
Engine	Rolls-Royce Kestrel IIIS	BMW VI 7.3 (703)	Hispano-Suiza 12 Xbrc (Ybre?)
Power	391 kW (525 hp)	485 kW (650 hp)	515 kW (690 hp)
Dimensions	Length: 10.60 m (34 ft 9 in) Height: 4.30 m (14 ft 1 in) Wingspan: 15.00 m (49 ft 3 in) Wing area: 32.40 m2 (349 ft2)	Length: 10.50 m (34 ft 5 in) Height: 4.44 m (14 ft 7 in) Wingspan: 15.00 m (49 ft 3 in) Wing area: 32.40 m2 (349 ft2)	Length: 10.60 m (34 ft 9 in) Height: 4.30 m (14 ft 1 in) Wingspan: 15.00 m (49 ft 3 in) Wing area 32.40 m2 (349 ft2)
Weights	Empty: 1,600 kg (3,530 lb) Loaded: 2,300 kg (5,070 lb) Max takeoff: 2,300 kg (5,070 lb)	Empty: 2,200 kg (4,850 lb) Loaded: 2,640 kg (5,820 lb) Max takeoff: 2,640 kg (5,820 lb)	Empty: 1,600 kg (3,530 lb) Loaded: 2,640 kg (5,820 lb)
Performance	Max. speed: 278 km/h (150 kn) at sea level Max. speed: 315 km/h (170 kn) at 3,500 m (11,500 ft) Range: 800 km (430 nmi) Service ceiling: 9,100 m (29,900 ft) Wing load: 71.0 kg/m2 (14.5 lb/ft2)	Max. speed: 288 km/h (179 mph) at sea level Cruising speed 250 km/h (135 kn) Climb to 1000 m: 1 min 54 s Climb to 5000 m: 12 min 48 s Initial climb rate : 8.80 m/s (1730 ft/min) Range: 800 km (430 nmi) Service ceiling: 7,500 m (24,600 ft) Wing load: 81.0 kg/m2 (16.6 lb/ft2)	Max. speed: 272 km/h (147 kn) at sea level Max. speed: 318 km/h (172 kn) at 3500 m Range: 800 km (430 nmi) Service ceiling: 9,500 m (31,200 ft)
Armament	Four × MG 08/15 machine guns (two forward, two in rear turret)

Sources

• Luftwaffe 39-45 Archived 2017-01-31 at the Wayback Machine (in Portuguese)
• Histaviation.com Archived 2015-01-26 at the Wayback Machine
• Virtual Aviation Museum

Notes

Bibliography

• Green, William and Swanborough, Gordon. The Complete Book of Fighters. New York: Smithmark, 1994. ISBN 0-8317-3939-8.

(Information on this model is difficult to come by and the nature of the relationship between C1/C4/10 is not yet totally resolved)