Mikoyan-Gurevich 23-01

Note: Not to be confused with the Mikoyan-Gurevich MiG-23, which was a completely different aircraft, though designed to fulfil the same specification.

Mikoyan-Gurevich 23-01
a 2-view of the 23-01
Role Mikoyan-Gurevich 23-01
National origin USSR
Manufacturer OKB Mikoyan-Gurevich
Designer V A Mikoyan (project manager)
First flight 3 April 1967
Developed from Mikoyan-Gurevich 23-31 / Izdeliye 92

The Mikoyan-Gurevich 23-01, aka Izdeliye 92 and (erroneously) Mikoyan-Gurevich MiG-23PD, NATO reporting name Faithless, was a 1960s STOL fighter / attack aircraft, designed in the USSR, to fulfil a requirement for ground-attack and fighter aircraft able to operate from short runways.

Specifications (23-01)

Data from Soviet X-Planes[1]

General characteristics

  • Crew: 1
  • Length: 16.8 m (55 ft 1 in) (excl. PVD boom)
  • Wingspan: 7.72 m (25 ft 4 in)
  • Wing area: 40 m2 (430 sq ft)
  • Empty weight: 12,020 kg (26,500 lb)
  • Gross weight: 16,000 kg (35,274 lb)
  • Powerplant: 1 × Tumansky R-27-300 afterburning turbojet engine, 76.49 kN (17,196 lbf) with afterburner
  • Powerplant: 2 × Rybinsk RD-36-35 turbojet engines, 46.09 kN (10,362 lbf) thrust each lift engines for STOL operations only

Performance

  • Take-off run: 180–200 m (591–656 ft) at light AUW
  • Landing run: 250 m (820 ft) with brake parachute

Armament

  • Missiles: displayed with dummy Vympel R-23R and R-23T missiles on two underwing pylons

Avionics
Provision for a large fire-control radar in the nose

References
  1. Gordon, Yefim; Gunston, Bill (2000). Soviet X-Planes. Hinkley: Midland. pp. 118–119. ISBN 978-1-85780-099-9.
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