Anatra Anadis
| {{Infobox Aircraft Begin
| name=Anatra Anadis | image=Anadis Fighter.jpg | caption= }}{{Infobox Aircraft Type | type=Fighter | national origin= Russian Empire | manufacturer=Anatra | designer=Elisee Alfred Descamps | first flight=23 October 1916{{ref book osprey encyc of russian aircraft|1}} | introduced= | retired= | status= | primary user= | number built=1 | developed from=Anatra Anasal | variants with their own articles= }} |
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 streamlined fuselage, the lack of a rear seat in the Anadis, plans for a forward-firing gun (not implemented) and a different engine.{{cite book|title=History of aircraft construction in the USSR until 1938 (Vol 5)|author=V. Shavrov|language=ru|date=2002|isbn=978-5217031122|publisher=Mashinostroenie}}
Development
In the spring of 1916, Elisee Alfred Descamps, a French designer and chief engineer of the Anatra company of Odessa was ordered to build a single-seat fighter based on the Anasal two-seat reconnaissance biplane. Retaining the Anasal's two-bay configuration and fabric-covered wooden construction, the fighter, dubbed the Anadis, differed in having a streamlined fuselage, the rear cockpit removed, provision made for forward-firing armament and the 150 hp Salmson water-cooled radial engine replaced by a similarly-rated Hispano-Suiza V8 water-cooled engine.
The prototype Anadis was flown on 23 October 1916 by the factory test pilot, another Frenchman, Jean Robinet. 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. Their plan was discovered by one Lieutenant Kononenko, an Imperial Army acceptance pilot attached to Anatra, and the modifications were reverted. Testing continued until 11 November 1916, the official report to the Imperial Army stating that it was "... not inferior to any German aircraft of the same type and with greater power".
Nevertheless, no further examples were ordered and the tested aircraft remained at the factory until the autumn of 1917. In September 1917, Staff Captain N.A. Makarov applied for permission to fly the aircraft on a long-distance propaganda flight along the route Odessa-Thessaloniki-Rome-Marseille-Paris with a subsequent return to Russia in order "to visit the fronts and factories, to see the Allied aviation... so that the Allies would supply us better". The flight was authorized. On 14 October, the Anadis was tested with a load of 500 kg. Interestingly, in addition to the identifying Russian cockades, the Anadis was painted very picturesquely: a two-headed eagle with the flags of the Entente countries were drawn on the fuselage and half-naked girls on the wings.{{cite book|title=Russian Aeroplanes 1914-1918|author=Mikhail Maslov|date=2002|publisher=Icarus Aviation Pubns|isbn=978-0972452700}}
In November 1917, Makarov went on the flight, but he crashed near the city of Iași in Romania due to an engine failure. The subsequent history of the aircraft is unknown.
Specifications
{{Aircraft specs
|ref=The Complete Book of Fighters{{cite book|author-last1=Green|author-first1=William|author-last2=Swanborough|author-first2=Gordon|date=1994|title=The Complete Book of Fighters|publisher=Salamander Books|isbn=9780861016433|url=https://archive.org/details/completebookoffi0000gree_d6t1/page/18/mode/1up?q=anadis|page=18}}
|prime units?=met
|crew=1
|capacity={{cvt|500|kg|0}} payload
|length m=7.75
|length note=
|span m=11.4
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|height m=
|height note=
|wing area sqm=37
|wing area note=
|aspect ratio=
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|empty weight kg=665
|empty weight note=
|gross weight kg=1165
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|eng1 number=1
|eng1 name=Hispano-Suiza 8A
|eng1 type=V-8 water--cooled piston engine
|eng1 hp=150
|eng1 note=
|prop blade number=2
|prop name=fixed-pitch propeller
|prop dia m=
|prop dia note=
|max speed kmh=153
|max speed note=
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|never exceed speed kmh=
|never exceed speed note=
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|ceiling m=
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|climb rate ms=2.22
|climb rate note=
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|wing loading kg/m2=29.7
|wing loading note=
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|power/mass=0.13 hp/kg
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}}
References
{{Commons category}}
{{reflist}}
{{Anatra aircraft}}
Category:1910s Russian fighter aircraft