Yakovlev Yak-23

Source: Wikipedia, the free encyclopedia.
Yak-23
Polish Yak-23 in the Lubuskie Muzeum Wojskowe, Drzonów
Role Fighter aircraft
Manufacturer Yakovlev
First flight 8 July 1947
Introduction 1949
Retired Early 1960s
Primary users Soviet Air Forces
Polish Air Force
Romanian Air Force
Czechoslovak Air Force
Bulgarian Air Force
Produced October 1949–January 1951
Number built 316 + 3 prototypes
Developed from Yakovlev Yak-17

The Yakovlev Yak-23 (

swept-wing Mikoyan-Gurevich MiG-15. Many Yak-23s were exported to the Warsaw Pact
nations and remained in service for most of the 1950s, although some were still in use a decade later.

Development and description

Yakovlev Yak-23UTI

On 11 March 1947, the

Alexander Yakovlev decided to develop two designs, the Yakovlev Yak-25 in accordance with the Ministry's order and a lightweight, more agile aircraft (the Yak-23) in the hopes that one or the other would win an order from the Ministry. Yakovlev's decision was a risky one as it could be construed as unauthorized use of state monies if discovered, which could have landed Yakovlev in a lot of trouble.[2]

To minimize risk, the new aircraft used the same "pod-and-boom" layout as the earlier Yak-17 fighter, but the metal

wingtips. The fighter was armed with two 23-millimeter (0.9 in) Nudelman-Rikhter NR-23 autocannon, each with 90 rounds.[3]

Two

Lieutenant Colonel Mikhail Ivanov, at the controls. While still involved in its manufacturer's flight testing, the first prototype participated in the flypast at Tushino Airfield on 3 August. The Yakovlev OKB concluded its testing on 24 September and turned over the second prototype for state acceptance trials on 22 October. Although the Yak-23 was accepted for series production, it was criticized of heavy aileron and rudder forces, lack of cockpit pressurization and heating and ventilation, protection for the pilot and weak armament. The test pilots did praise it as highly maneuverable, with a good acceleration and takeoff and climb capabilities thanks to a high thrust-to-weight ratio. The second prototype was modified afterwards to address some of these issues and successfully tested again in 1948.[4]

Operational history

Romanian Yak-23s at Ianca

The first aircraft were produced in a factory in

trainer
which appears to have had the unusual arrangement of having the instructor seated in front of the student, and the Yak-23DC trainer which was produced in Romania.

Small numbers of Yak-23s were exported to Czechoslovakia (20 from 1949, named S-101), Bulgaria (from 1949), Poland (about 100, from 1950), Romania (62, from 1951). Poland and Czechoslovakia acquired licenses for the aircraft, but built the superior MiG-15 instead. Yak-23s were withdrawn by the late 1950s, except in Romania which used them until 1960.[5]

A Romanian Yak-23 flown by Major Dumitru Balaur successfully intercepted a Soviet Ilyushin Il-28 on the night of 28 October 1952. Being tracked from the ground on radar, the Il-28 was intercepted by the Yak-23 fighter scrambled from the Ianca airfield after it had passed into the Romanian airspace a second time. As the bomber refused to follow the Romanian pilot's instructions, the fighter moved into position to shoot it down but was recalled to base. This was the first interception mission carried out by the Romanian Air Force.[6]

U.S. testing

A single Yak-23 was acquired by US intelligence via

F-86 Sabres whose pilots inquired as to the plane's identity. A story was conceived that the aircraft was a Bell X-5
, which had a similar layout. At the completion of design and flight evaluations the aircraft was again disassembled and shipped quietly back to Yugoslavia in its original paint scheme.

Records

On September 21, 1957, the Polish pilot Andrzej Abłamowicz set two FAI world records in the Yak-23 with civilian markings SP-GLK, in its weight class, climbing to 3,000 m (9,843 ft) in 119 seconds (4,962.6 ft/min, 25,21  m/s) and to 6,000 m (19,685 ft) in 197 seconds (5,995.4 ft/min, 30,45 m/s). This plane was withdrawn in 1961.

Variants

  • Yak-23: Fighter version, serial built.
  • Yak-23UTI: Two-seat training version with longer fuselage and lighter armament, three built.
  • Yak-23DC: Romanian-built two-seat training version. Four Yak-23 single-seaters were converted in 1956 by ASAM Pipera, two of them belonging to the Bulgarian AF.
  • S-101: Czechoslovak designation.

Operators

Monino Airfield
Kbely
(marked HX-51)

 Albania

 Bulgaria

 Czechoslovakia

 North Korea

 Poland

 Romania

 Soviet Union

  • Soviet Air Force
    - Operated aircraft between 1949 and 1951.

Specifications (Yak-23)

Yak-23 3-view drawing

Data from The Complete Book of Fighters[9]

General characteristics

  • Crew: 1
  • Length: 8.13 m (26 ft 8 in)
  • Wingspan: 8.73 m (28 ft 8 in)
  • Height: 3.31 m (10 ft 10 in)
  • Wing area: 13.5 m2 (145 sq ft)
  • Empty weight: 1,980 kg (4,365 lb)
  • Gross weight: 3,384 kg (7,460 lb)
  • Powerplant: 1 × Klimov RD-500 centrifugal-flow turbojet engine, 15.6 kN (3,500 lbf) thrust

Performance

  • Maximum speed: 925 km/h (575 mph, 499 kn) at sea level
  • Range: 1,200 km (750 mi, 650 nmi)
  • Service ceiling: 14,800 m (48,600 ft) [10]
  • Rate of climb: 47 m/s (9,300 ft/min) [10]
  • Thrust/weight: 0.46

Armament

See also

Aircraft of comparable role, configuration, and era

Related lists

References

  1. ^ Parsch, Andreas; Martynov, Aleksey V. "Designations of Soviet and Russian Military Aircraft and Missiles". www.designation-systems.net. Retrieved 21 January 2017.
  2. ^ Gordon & Kommissarov 2014, pp. 156–57.
  3. ^ Gordon & Kommissarov 2014, pp. 204–11.
  4. ^ Gordon & Kommissarov 2014, pp. 164–65, 168.
  5. ^ Paul Sandachi (2001). Aviația de luptă reactivă în România: 1951 - 2001. Muzeul Aviației. p. 25.
  6. ^ "Prima misiune de interceptare a unei ținte reale în cadrul Forțelor Aeriene Române". aviatiamagazin.com (in Romanian). 28 October 2014.
  7. ^ "JEDNA OD NAJVEĆIH TAJNI TITOVE JUGOSLAVIJE: Projekat Alfa- slanje sovjetskih mlaznjaka u SAD".
  8. ^ a b "Samolotypolskie.pl - Jakowlew Jak-23".
  9. ^ Green and Swanborough 1994, pp. 604–605.
  10. ^ a b Gunston 1995, p. 478.

Bibliography

External links