| 词条 | Anatra Anadis | |||||||||||||||
| 释义 |
The Anatra Anadis was developed in 1916 as a single-seat fighter variant of the Anatra Anasal reconnaissance biplane. The main difference between the two aircraft was the lack of a rear seat in the Anadis, plans for a forward-firing gun (not implemented) and a different engine. DevelopmentAfter the aircraft flew for the first time on 23 October 1916, the test pilot and designer modified the fighter to recover the second seat and carry extra fuel tanks, the idea being to use it to escape Russia in the event of the impending revolution.[1] Their plan was discovered and the modifications were reverted. Testing continued until 11 November 1916. Despite glowing reports of the aircraft's performance, none were ordered and the prototype sat at the factory until October 1917. On the 14th the aircraft took off on a flight tour of Europe and crash landed in Romania.[1] That was the only known aircraft and there are no known photographs.[4] Specifications{{aircraft specifications|plane or copter?=plane |jet or prop?=prop |ref=[2] |crew=1 |capacity= |payload main=500kg |payload alt=1102lb |payload more= |length main= 7.75m |length alt=24ft 7in |span main=11.40m |span alt=37ft 5in |height main= |height alt= |area main= 37 m2 |area alt= 398ft2 |airfoil= |empty weight main= 665kg |empty weight alt= 1466 |loaded weight main= 1165kg |loaded weight alt= 2568lb |useful load main= |useful load alt= |max takeoff weight main= |max takeoff weight alt= |max takeoff weight more= |more general= |engine (jet)= |type of jet= |number of jets= |thrust main= |thrust alt= |thrust original= |afterburning thrust main= |afterburning thrust alt= |thrust more= |engine=prop |type of prop=Hispano-Suiza water-cooled V-8 |number of props=1 |power main= 150hp |power alt=112kW |power original= |power more= ||propeller or rotor?=propeller |propellers=1 |number of propellers per engine= |propeller diameter main= |propeller diameter alt= |max speed main= 153 km/h |max speed alt=95 mph |max speed more= |cruise speed main= |cruise speed alt= |cruise speed more |stall speed main= |stall speed alt= |stall speed more= |never exceed speed main= |never exceed speed alt= |range main= |range alt= |ferry range main= |ferry range alt= |ferry range more= |ceiling main= |ceiling alt= |climb rate main= 133.3 m/min |climb rate alt= 437 ft/min |loading main= |loading alt= |thrust/weight= |power/mass main= |power/mass alt= |more performance= |armament= |guns= |bombs= |rockets= |missiles= |hardpoints= |hardpoint capacity= |avionics= }}{{aircontent |see also= |related= |similar aircraft= |lists= }} References{{commons category|Anatra aircraft}}1. ^1 2 {{ref book osprey encyc of russian aircraft|1}} 2. ^1 Green, William; Swanborough, Gordon. "Anatra Andis" (1998), The Complete Book of Fighters. Salamander Books, Spain 4 : Russian fighter aircraft 1910–1919|Anatra aircraft|Single-engined tractor aircraft|Biplanes |
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