avia.wikisort.org - Aeroplane

Search / Calendar

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.

Do 10
Role Fighter aircraft
National origin Germany
Manufacturer Dornier Flugzeugwerke
First flight 24 July 1931[1]

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
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


Wikimedia Commons has media related to Dornier Do 10.
Notes
  1. Green and Swanborough 1994, p. 185.
Bibliography

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


На других языках

[de] Dornier Do 10

Die Dornier Do 10 war ein einmotoriges zweisitziges Jagdflugzeug der deutschen Dornier-Werke.
- [en] Dornier Do 10

[fr] Dornier Do 10

Le Dornier Do 10 (aussi appelé Do C1 ou Do C4 initialement) est un prototype de chasseur biplace et monomoteur conçu par l'avionneur allemand Dornier Flugzeugwerke au tout début des années 1930. Il n'est construit qu'à deux exemplaires.

[it] Dornier Do 10

Il Dornier Do 10 era un caccia monomotore ad ala alta a parasole sviluppato dall'azienda tedesca Dornier-Metallbauten GmbH nei primi anni trenta e rimasto allo stadio di prototipo.


Текст в блоке "Читать" взят с сайта "Википедия" и доступен по лицензии Creative Commons Attribution-ShareAlike; в отдельных случаях могут действовать дополнительные условия.

Другой контент может иметь иную лицензию. Перед использованием материалов сайта WikiSort.org внимательно изучите правила лицензирования конкретных элементов наполнения сайта.

2019-2025
WikiSort.org - проект по пересортировке и дополнению контента Википедии