The Antonov A-1 and related designs were a family of single-seat training gliders produced in the Soviet Union in the 1930s and 1940s. All were derived from the Standard-2 (Стандарт-2) (designed and flown by
Oleg Konstantinovich Antonov
Oleg Konstantinovich Antonov (russian: Оле́г Константи́нович Анто́нов; 7 February 1906 – 4 April 1984) was a Soviet aeroplane designer, and the founder of the Antonov Design Bureau (located in Kyiv, Ukraine), named ...
in 1930
[Sheremetev 1959, 20]), which in turn was derived from the Standard-1.
[Krasil'shchikov 1991, 145] They were produced in large numbers, with around 5,400 built of the U-s3, U-s4 and P-s2 major versions alone.
[Central Museum of the Air Force] The same design formed the basis for the
Antonov A-2 __NOTOC__
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 num ...
and its related group of two-seat designs. Altogether, including the two-seaters, production exceeded 7,600 by 1937.
[Krasil'shchikov 1991, 143]
While members of the family varied in detail, they shared the same basic design, and parts were interchangeable between them.
[Shushurin 1938, 13] The design featured a typical primary glider layout with a conventional
empennage
The empennage ( or ), also known as the tail or tail assembly, is a structure at the rear of an aircraft that provides stability during flight, in a way similar to the feathers on an arrow.Crane, Dale: ''Dictionary of Aeronautical Terms, third ed ...
carried at the end of a long boom in place of a conventional
fuselage
The fuselage (; from the French ''fuselé'' "spindle-shaped") is an aircraft's main body section. It holds crew, passengers, or cargo. In single-engine aircraft, it will usually contain an engine as well, although in some amphibious aircraft t ...
. The boom could be folded sideways for storage.
[Shushurin 1938, 16] The monoplane wing was carried high on a pylon above this "keel" and was further braced to it with two struts on either side.
[Sheremetev 1959, 21–22] The pilot sat in front of the wing, and was enclosed in a simple U-shaped wooden fairing that was removed by sliding it forward to allow him or her to enter and leave the aircraft.
[Sheremetev 1959, 40] The undercarriage consisted of a single skid underneath the "keel", but this could also be fitted with small wooden wheels.
[Sheremetev 1959, 42]
While the original primary training versions (designated У, 'U') featured wings of constant chord,
subsequent variants designed for soaring flight (designated П, 'P') had longer-span wings with tapering outer panels and a streamlined nose fairing.
[Krasil'shchikov 1991, 146] The ultimate development in the line were gliders intended for towed flight (designated Б, 'B), which shared the longer wings and streamlined fairing of the P-types, but added a canopy to enclose the cockpit.
Unlicensed copies were produced in Turkey following World War II by
THK and ''Makina ve Kimya Endüstrisi Kurumu'' (MKEK), as the THK-7 (P-s2) and THK-4 (U-s4).
[Deniz 2004]
Variants
In each case, the "s" stands for ''serii'' (серии: 'series')
Prototypes
:Standard-1 (Стандарт-1)
:Standard-2 (Стандарт-2)
Trainers
''Uchebnyi'' (Учебный, 'Trainer')
:U-s1 (У-с1)
:U-s2 (У-с2) (First version built in series
)
:U-s3 (У-с3) (1,600 built
)
:U-s4 (У-с4) (Redesignated A-1, major production version. 3000 built
)
Sailplanes
''Paritel'' (Паритель, 'Sailplane'), also ''Upar'' (Упар, portmanteau of учебный паритель, ''uchebnyi paritel'', 'training sailplane') (800 built
)
:P-s1 (П-с1)
:P-s2 (П-с2)
Towed
''Buksirovochnye'' (Буксировочные, 'Towed') (265 built by 1937
)
:B-s3 (Б-с3)
:B-s4 (Б-с4)
:B-s5 (Б-с5)
Specifications (A-1)
Notes
References
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{{MKEK aircraft
1930s Soviet sailplanes
Glider aircraft
A-01
Aircraft first flown in 1930