Antonov A-2
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{{Infobox Aircraft Begin
| name=A-2 | image= | caption= }}{{Infobox Aircraft Type | type=Training glider | national origin=USSR | manufacturer= | designer=Oleg Konstantinovich Antonov | first flight=1936 | introduced= | retired= | status= | primary user= | number built=ca. 2,300 | developed from= | variants with their own articles= }} |
The Antonov A-2 and related designs were a family of two-seat training gliders produced in the Soviet Union in the 1930s and 1940s, all derived from the single-seat Antonov A-1 family.Sheremetev 1959, 44 They were produced in large numbers, with at least 2,300 built by 1937, and together with the single-seaters, production exceeded 7,600 by the same year.Krasil'shchikov 1991, 143
Like the A-1, the A-2 was a minimalist primary glider, with a conventional tail mounted on a boom and a strut-braced monoplane wing, mounted parasol-fashion. However, while the single-seat primary gliders featured wings of constant chord, the two-seaters used the longer-span, tapered wings that had been developed for the soaring versions of the single-seat family (P-s1 and P-s2).Sheremetev 1959, 45 The other major difference was the design of the cockpit gondola. The single-seaters featured an aerodynamic fairing that slid on and off to provide access to the pilot's seat.Sheremetev 1959, 40 The two-seaters, however, had a permanently fixed cockpit pod that seated the pilot and instructor in tandem, open cockpits, each with a small windscreen The rear cockpit was located directly beneath the wing and was accessed via a door on the port side of the gondola. Apart from the change in gondola, all other components remained interchangeable with the Ps-2Shushurin 1938, 67
Variants
In each case, the "s" stands for serii (серии – "series")
Uchebnyi (Учебный – "Trainer")
- U-s5 (У-с5)
- U-s6 (У-с6)
Specifications (U-s5)
{{Aircraft specs
|ref=Shushurin 1938, 67
|prime units? = met
|crew=two, pilot and instructor
|length m=5.80
|length ft=19
|length in=0
|span m=13.80
|span ft=45
|span in=3
|height m=1.70
|height ft=5
|height in=7
|wing area sqm=17.1
|wing area sqft=184
|empty weight kg=120
|empty weight lb=264
|gross weight kg=264
|gross weight lb=581
|max speed kmh=70
|max speed mph=40
|sink rate ms=1.1
|sink rate ftmin=220
}}
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Notes
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References
- {{cite book |last=Krasil'shchikov |first=Aleksandr Petrovich |title=Planery SSSR (Gliders of the USSR) |year=1991 |publisher=Moskva Mashinostroyeniye |location=Moscow}}
- {{cite book |last= Sheremetev |first= Boris Nikolayevich |title=Planery (Gliders) |year=1959 |publisher=DOSAAF |location=Moscow }}
- {{cite book |last= Shushurin |first=V.V. |title=Atlas konstruktzii planerov (Directory of glider construction) |year=1938 |publisher=Gosudarstvennoe izdatel'stvo oboronnoi promyshlennosti |location=Moscow }}
{{Antonov aircraft}}
Category:1930s Soviet sailplanes