| 词条 | DAR 10 | |||||||||||||||||
| 释义 |
The DAR 10 (ДАР 10) was a Bulgarian light bomber and reconnaissance aircraft. DAR-10 was designed for horizontal and dive bombing, reconnaissance, and ground attack. Design and developmentThe DAR 10 was designed by Zvetan Lazarov in 1938 in the DAR (Darzhavna Aeroplanna Rabotilnitsa, meaning literally 'State Airplane Workshop') factory in Bozhurishte, near the capital Sofia. The DAR 10 was a single-engine two-seat (pilot and gunner) low-wing cantilever monoplane aircraft of conventional layout. Its two seats were in tandem under enclosed glazing. Its tailwheel undercarriage was fixed, and the mainwheels were spatted. The wings had a wooden structure, covered with plywood. Flaps were not used. The fuselage was comparatively wide and deep, to accommodate the nose-mounted radial engine. It was constructed of steel-tube framework and wood formers, covered with fabric. Three-bladed steel propellers were used. Two prototypes were built, powered by different engines:
This aircraft crashed in October 1942.[1] In spite of good flight reviews, the type was not chosen for production. The high-wing KB-11 Fazan was selected for production instead.
The DAR-10 was not selected for production. Some sources suggest that it was passed over in favor of the German Junkers Ju 87 Stuka dive bomber, while the improved DAR-10F was not selected as World War II had ended and Bulgaria had access to ample supplies of modern Soviet aircraft such as the Ilyushin Il-2 and Il-10.[1] Variants
First prototype, powered by an Alfa Romeo radial engine.
Second prototype, powered by a Fiat radial engine. Operators
Specifications (DAR-10){{aircraft specifications/switch
|plane or copter?=plane |jet or prop?=prop
|ref=Jane's Aircraft Recognition Guide [2]
|crew=two |length main=9.54 m |length alt=31.3 feet |span main=12.20 m |span alt=40.0 feet |height main=3.3 m |height alt=10.8 feet |area main=22.2 m² |area alt=239 ft² |empty weight main=1,843 kg |empty weight alt=4,063 lb |loaded weight main=2,570 kg |loaded weight alt=5,666 lb |useful load main= |useful load alt= |max takeoff weight main= |max takeoff weight alt=
|engine (prop)=Alfa Romeo 128 R.C.21 |type of prop= |number of props=1 |power main=708 kW |power alt=950 hp
|max speed main=410 km/h |max speed alt=255 mph |max speed more= |never exceed speed main= |never exceed speed alt= |range main=1,170 km |range alt=727 miles |ceiling main=7,250 m |ceiling alt=23,785 feet |climb rate main= |climb rate alt= |loading main= |loading alt= |thrust/weight=
|armament=
}} See also{{aircontent|related= |similar aircraft=
|lists=
|see also= }} References1. ^1 2 3 4 Bernád 2001, p.29. 2. ^{{cite book|title=Jane's Aircraft Recognition Guide|last=Rendall|first=David|page=505|year=1995|isbn=0-00-470980-2|publisher=HarperCollinsPublishers|location=Glasgow, UK}}
External links{{commons category|DAR 10}}
8 : Single-engined tractor aircraft|Low-wing aircraft|Bulgarian bomber aircraft 1940–1949|Bulgarian military reconnaissance aircraft 1940–1949|DAR aircraft|World War II Bulgarian light bombers|World War II Bulgarian reconnaissance aircraft|Aircraft first flown in 1941 |
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