Sukhoi Su-22M4 Fitter-K Aircraft Data
The Sukhoi Su-22 (NATO reporting name: Fitter) is a Soviet variable-sweep wing fighter-bomber developed from the Sukhoi Su-7. It enjoyed a long career in Soviet, later Russian, service and was widely exported to Eastern Bloc, Arab air forces, Angola and Peru as the Su-22. It is the first variable-sweep wing of Russian/Soviet origin
The Su-22MR Fitter-K is the final production version with considerably upgraded avionics, including RSDN navigation (similar to LORAN), beacon navigation, inertial navigation, a more powerful (Klyon) "Kлён-54" laser rangefinder, radio compass, and SPO-15LE ("Sirena") radar-warning system. Additional fuselage inlets (including ram-air inlet at the base of the fin) to improve engine cooling airflow, and a fixed air intake shock cone. Many aircraft were equipped for the use of TV-guided missiles and BA-58 Vjuga pod for anti-radiation missiles. AL-21F-3 engine. Export version was designated Su-22M4 (factory S-54K). First flight: 19 June 1980 with Yu. A. Yegorov at the controls. Su-17M4 was manufactured 1981–1988, Su-22M4 was manufactured 1983–1990.
The Su-22MR Fitter-K is the final production version with considerably upgraded avionics, including RSDN navigation (similar to LORAN), beacon navigation, inertial navigation, a more powerful (Klyon) "Kлён-54" laser rangefinder, radio compass, and SPO-15LE ("Sirena") radar-warning system. Additional fuselage inlets (including ram-air inlet at the base of the fin) to improve engine cooling airflow, and a fixed air intake shock cone. Many aircraft were equipped for the use of TV-guided missiles and BA-58 Vjuga pod for anti-radiation missiles. AL-21F-3 engine. Export version was designated Su-22M4 (factory S-54K). First flight: 19 June 1980 with Yu. A. Yegorov at the controls. Su-17M4 was manufactured 1981–1988, Su-22M4 was manufactured 1983–1990.
- Country of Origin: Soviet Union
- First Flight: 1983
- Initial Service Date: 1983
- No. Built: 771
- No. In Service: 150 (approx.)
- No. of Hardpoints: 12
- Crew: 1
Power:
1 × Lyulka AL-21F-3 afterburning turbojet at 17,185 lbf or Thrust with afterburner: at 24,675 lbf
Weapons:
Guns:
2 × 30 mm Nudelman-Rikhter NR-30 autocannons (80 rounds per gun, 160 rounds total)
UPK-23 or SPPU-22 gun pods for 2 × Gryazev-Shipunov GSh-23L autocannons
Hardpoints: 12 hardpoints with a capacity of up to 4,000 kg (8,800 lb) of stores and provisions to carry combinations of:
Missiles:
Air-to-air missiles:
K-13
R-60
R-73
Air-to-surface missiles:
Kh-23 Grom
Kh-25ML
Kh-29L/T/D
Anti-radiation missiles:
Kh-58
Kh-27PS
Kh-28
Bombs: drop bombs, laser-guided bombs, electro-optical bombs, napalm bombs, drag chute bombs and cluster bombs
2 × 30 mm Nudelman-Rikhter NR-30 autocannons (80 rounds per gun, 160 rounds total)
UPK-23 or SPPU-22 gun pods for 2 × Gryazev-Shipunov GSh-23L autocannons
Hardpoints: 12 hardpoints with a capacity of up to 4,000 kg (8,800 lb) of stores and provisions to carry combinations of:
Missiles:
Air-to-air missiles:
K-13
R-60
R-73
Air-to-surface missiles:
Kh-23 Grom
Kh-25ML
Kh-29L/T/D
Anti-radiation missiles:
Kh-58
Kh-27PS
Kh-28
Bombs: drop bombs, laser-guided bombs, electro-optical bombs, napalm bombs, drag chute bombs and cluster bombs
Dimensions:
Length: | 62 ft 5 in. |
Wing Span: | 44 ft 11 in. |
Wing Area: | 414 sq.ft |
Height: | 16 ft 10 in. |
Empty Weight: | 26,810 lbs |
Max. Weight: | 42,835 lbs |
Max. Ordnance Load: | 36,155 lbs |
Internal Fuel: | 8,310 lbs |
Performance:
Max. Speed: | 870 mph |
Service Ceiling: | 46,590 ft. |
Normal Range: | 945 nm |
Max. Range: | 1,430 nm |