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  Wikipedia: Dornier Do 10

Wikipedia: Dornier Do 10
Dornier Do 10
From Wikipedia, the free encyclopedia.

The Dornier Do 10 was the name given by the Reichsluftfahrtministerium(RLM) of a pre-World War II German aircraft. The aircraft has a complicated history due to renaming and the use of three different engines with correspondingly different specifications.

Developed in 1931, it was originally called Do C1, with one variant being the C4. It was the first aircraft of the C model line and was followed by the by the C2. It most likely started as the C1 and performacne numbers suggest it tested BMW engine tilted and then Hispano-Suiza powerplants. Later that year possibly renamed C4 with the testing of the Rolls-Royce engine. The tilted engine and propeller postion was one of the key features it tested along with multiple engine use. In any case, it was a two-seat parasol monoplane intended to be used as a fighter. Two protoypes were made both in 1931.

Specifications

 
   

 
   
Type Two seat fighter
Engine 1 Rolls-Royce Kestrel IIIS 1 BMW VI 7.3 (703) 1 Hispano-Suiza 12 Xbrc(Ybre?)
Horsepower 525hp 650hp 690hp
Dimensions Length: 10.60 m ( 34.777 ft)
height: 4.30 m (14.108 ft)
wingspan: 15.00 m (49.213 ft)

   
wing area: 32.40 m2(348.754 sqft)
Length: 10.50 m(34.449 ft)
height: 4.44 m(14.567 ft)
wingspan: 15.00 m(49.213 ft)
wing area: 32.40 m2(348.754 sqft)
Length: 10.60 m
height: 4.30 m
wingspan: 15.00 m wing area 32.40 m2
Weights Empty weight: 1600kg (3528.0 lbs)
max take off weight: 2300.0 kg(5071.5lbs)
flying weight: 2300kg
Empty weight: 2200kg(4851.0lbs)
flying weight: 2640
max take off weight: 2640.0kg (5821.2 lbs) kg
Empty: 1600kg
flying weight: 2640kg
Performance Max. speed: 278 km/h (170 kts) at sea level
315 km/h at
   3500 m
range: 800 km(432 nm)

service ceiling: 9100m(29856 ft )
Wing load: 71.00 kg/m^3 (14.56 lbs/ft^2)
  
Max. speed: 288 km/h (156 kts) at sea level
cruising speed 250 km/h(135 kts)
climb to 1000 m: 1 min. 54 sec.
to 5000m: 12 min. 48 sec.
Initial climb rate : 8.80 m/s(1732.28 ft/min)
range: 800 km
service ceiling: 7500 m
Wing load : 16.61 81.00 kg/m^2 (lbs/ft^2)
Max. speed: 272 km/h at sea level
318 km/h at 3500 m
Range: 800 km
Service ceiling: 9500m
Armament Four MG 08/15, (two forward, two in rear turret)
(nm=nautical miles, kts= knots)

Informatio Sources: (Limited information) [1 ] (This site has good picture of the tilted engine) [2] (non-english, must use online site tranlator to view english) Best site, lot of information found here. Although aircraft pictured does not appear to have tilted engine)'' [3] Another data source: [4]

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


  

From Wikipedia, the free encyclopedia. 
Modified by Geona