Wikipedia

Yakovlev Yak-23

(Redirected from Yak-23)

The Yakovlev Yak-23 (Russian: Яковлев Як-23; USAF/DoD reporting name Type 28, NATO reporting name Flora)[1] is an early Soviet jet fighter with a straight wing. It was developed from the Yak-17 in the late 1940s and used a reverse-engineered copy of a British engine. It was not built in large numbers as it was inferior in performance to the 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.

Yak-23
Polish Yak-23 in the Lubuskie Muzeum Wojskowe, Drzonów
General information
TypeFighter aircraft
ManufacturerYakovlev
Primary usersSoviet Air Forces
Number built316 + 3 prototypes
History
ManufacturedOctober 1949–January 1951
Introduction date1949
First flight8 July 1947
RetiredEarly 1960s
Developed fromYakovlev Yak-17

Development and description

edit
 
Yakovlev Yak-23UTI

On 11 March 1947, the Council of People's Commissars ordered several design bureaux (OKB), including that of Alexander Yakovlev, to develop a single-seat, straight-winged jet fighter to be equipped with a single British Rolls-Royce Nene or Rolls-Royce Derwent turbojet engine. The aircraft should have a maximum speed of 950 kilometers per hour (590 mph) at sea level and a speed of 1,000 km/h (621 mph) at an altitude of 5,000 meters (16,400 ft). It should be able to climb to that altitude in 3.5 minutes or less and should have a maximum range of no less than 1,200 kilometers (750 mi). 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 fuselage was redesigned as a semi-monocoque structure with the single-seat, unpressurized cockpit and its teardrop-shaped canopy positioned just above the trailing edge of the wing. Not coincidentally, this was also above the exhaust of the 1,590-kilogram-force (15.6 kN; 3,500 lbf) centrifugal-flow Klimov RD-500 engine, an unlicensed copy of the Derwent V. Fitted with tricycle landing gear, the main landing gear retracted inwards into the fuselage while the nose gear retracted forwards. Unlike the installation in the Yak-17, the Yak-23's forward landing gear was flush with the fuselage when retracted. The laminar-flow, two-spar, wing was mounted in the middle of the fuselage. It was equipped with slotted flaps and ailerons and had a modest 3° 30' dihedral. The horizontal stabilizers had 5° of dihedral. The pilot was protected by a bulletproof windscreen and the armored back of the ejection seat. The Yak-23 was equipped with five non-self-sealing fuel tanks in the fuselage that had a total capacity of 910 liters (200 imp gal; 240 U.S. gal) of fuel. In addition it could carry a pair of 195-liter (43 imp gal; 52 U.S. gal) drop tanks under the wingtips. The fighter was armed with two 23-millimeter (0.9 in) Nudelman-Rikhter NR-23 autocannon, each with 90 rounds.[3]

Two prototypes and a static-test airframe were ordered and the aircraft first flew on 8 July 1947 with the Hero of the Soviet Union, 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

edit
 
Romanian Yak-23s at Ianca

The first aircraft were produced in a factory in Tbilisi in October 1949. In late 1949 they entered Soviet air force service. The Yak-23 was quickly replaced in the Soviet service with the more complicated swept-wing MiG-15, which offered superior performance. In all, only 316 Yak-23 aircraft were built before production ended in 1951. Apart from the fighter there were two trainer versions of the Yak-23 which were built in small numbers. The Yak-23UTI two-seat 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

edit

A single Yak-23 was acquired by US intelligence via Yugoslavia in November 1953. The aircraft was a Romanian Yak-23 flown by Mihail Diaconu who had defected with it. The aircraft arrived disassembled and was shipped to the U.S. Air Force Test and Evaluation Center at Wright Field near Dayton, Ohio.[7] It was reassembled and made operational for several test flights, during which time it was disguised with U.S. markings. Efforts were made to keep the aircraft's identity secret and it was flown only in the early morning. On one occasion it was passed on the runway by a formation of 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

edit

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

edit
  • 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

edit
 
Yak-23 in the Russian Central Air Force Museum, Monino Airfield
 
Czechoslovak Yak-23 at the Prague Aviation Museum, Kbely (marked HX-51)

  Albania

  Bulgaria

  Czechoslovakia

  North Korea

  Poland

  Romania

  Soviet Union

Specifications (Yak-23)

edit
 
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

edit

Aircraft of comparable role, configuration, and era

Related lists

References

edit
  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

edit
  • Gordon, Yefim & Kommissarov, Dmitry. Early Soviet Jet Fighters. Manchester, UK: Hikoki Publications, 2014. ISBN 978-1-90210935-0.
  • Green, William & Swanborough, Gordon.The Complete Book of Fighters. London: Salamander Books. 1994. ISBN 1-85833-777-1.
  • Gunston, Bill. The Osprey Encyclopedia of Russian Aircraft 1875–1995. London: Osprey, 1995. ISBN 1-85532-405-9.
  • Mikolajczuk, Marian. Yakovlev Yak-23: The First Yakovlev Jet Fighters. Sandomirez, Poland: Stratus, 2008. ISBN 978-83-89450-54-8.
edit
 
Wikimedia Commons has media related to Yakovlev Yak-23.
Retrieved from "https://en.wikipedia.org/w/index.php?title=Yakovlev_Yak-23&oldid=1253232493"