Yakovlev Yak-32

From Wikipedia, the free encyclopedia

This is an old revision of this page, as edited by 77.48.225.5 (talk) at 01:44, 15 January 2016 (→‎See also: added L-29 main Yak-30 competior to the similar planes. L-29A Akrobat was also civilian single seat aerobatic version.). The present address (URL) is a permanent link to this revision, which may differ significantly from the current revision.

Yak-32
Yak-32 on the MAKS airshow 2009
Role Sport Aircraft
Manufacturer Yakovlev
First flight 1960
Primary user Soviet Air Forces
Number built 3
Variants Yakovlev Yak-30 (1960)

The Yakovlev Yak-32 (NATO reporting name Mantis) was a single-seat version of the Yakovlev Yak-30 (1960), and was claimed by the OKB to be the world's first sporting aircraft with an ejection seat. This version was designated as Yak-104PS. Neither the Yak-30 or the Yak-32 entered production.[1]

Design and development

Developed concurrently with the Yak-30, the Yak-32 was a single-seat aircraft designed as both a sporting jet, and a light military ground attack aircraft.[1] The airframe of the Yak-32 was that of the Yak-30, but modified to include only a single seat.[1] Yakovlev had intended to market the aircraft as a sporting jet at a time when no other single-seat jet aircraft was being market for civilian use. In fact, it would not be until the introduction of the jet version of the Bede BD-5 in the 1970s that another sport aircraft like the Yak-32 was offered. Even in the 21st century single-seat sporting jets are rarely offered by manufacturers.

The light attack version of the Yak-32 was designated as Yak-32Sh, and was planned to include more sophisticated avionics than the Yak-32. It could also carry external fuel and weapons loads, including a ZB-500 or ZB-360 external fuel tank, bombs of up to 500 kg, up to four rocket launchers (the largest being the UB-32/S-5), up to four K-13/R-3S missiles, four ARS-240 rockets, or four AOI-9 or UKP-23 gun pods, each with 250 rounds.[1]

On 5 August 1971, one of the Yak-32 was ordered to be equipped with RU19P-300 which has been modified to permit longer inverted flight. The aircraft received the designation Yak-32P. Flight evaluation of the aircraft was just as good as the original Yak-32.

Operational history

Three Yak-32 prototypes were built in 1960-1961 at the same time as the four prototype Yak-30s trainers. They had callsigns 32, 60 and 70. The aircraft 30 and 70 gave aerobatic demonstrations at that 1961 Aviation Day at Tushino. They went on to set several world class records (their thrust being misreported to the FAI as 800 kg).[1]

The ASCC allocated the name "Mantis" to the Yak-32/Yak-104.[1]

Survivors

  • One Yak-32 was preserved by Yakovlev and is on display at Khodinka, displayed in the OKB's house colors of red and white.[citation needed]

Specifications (Yak-32)

Data from [1]

General characteristics

  • Crew: 1 Basic fuel capacity: 500 kg (1,102 lb)
  • Maximum fuel capacity: 805 kg (1,775 lb)
  • Max wing loading: 154 kg/m² (31.6 lb/ft²)
  • Max power loading: 0.41 kg/kgp (0.9 lb/lbp)

Performance

  • Thrust/weight: 0.36
  • Maximum endurance: 2.05 hr
  • Take off run: 425 m (1,394 ft)
  • Landing run: 450 m (1,476 ft)
  • Maximum load factor: +7/-5 g

Armament
Various

See also

Related development

Aircraft of comparable role, configuration, and era

References

Notes

  1. ^ a b c d e f g Gunston, William 'Bill'; Gordon, Yefim (1997). Yakovlev Aircraft since 1924. London, UK: Putnam Aeronautical Books. ISBN 978-1-55750-978-9.

Bibliography

  • Jakubovich, Nikolay. Wings of Motherland: Aviation and politics, or how 'Dolphin' destroyed Yak-30.

External links