|
Engine type |
Volvo Flygmotor RM6C (Rolls-Royce Avon 300 Mk. 60) |
|
Afterburner type |
EBK67 |
|
Maximum dry thrust (without afterburner) |
57 kN |
|
Maximum wet thrust (with afterburner) |
77 kN |
|
Maximum speed, clean aircraft @10000 m (30000 ft) |
Mach 2.0 |
|
Climb rate |
180–200 m per second |
|
Turn rate (sustained) |
12 per second |
|
Turn rate (instantaneous) |
20 per second |
|
Empty weight |
8183 kg |
|
MTO weight |
12430 kg |
|
Wing span |
9.42 m |
|
Length |
15.34 m |
|
Height |
3.89 m |
|
Wing area |
49.22 m2 |
|
Maximum wing load |
253 kg/m2 |
|
Takeoff runway length (with/without afterburner) |
790 m / 1200 m |
|
Landing runway length (with/without drag chute) |
880 m / 1220 m |
|
Fuel capacity (internal tanks) |
2865 l |
|
Fuel capacity (external tanks) |
2 x 525 l |
|
Gunsight |
Ericsson 7A |
|
Radar |
Ericsson PS-03/A |
|
Navigation |
Collins VOR/DME, ADF, Garmin GPS |
|
Communication |
FR31 VHF/UHF voice/data com FR21 VHF data/voice com |
|
Other equipment |
IFF transponder |
|
Armament |
2 x 30 mm M-55 Aden cannons 1–2 x AIM-9 P3/P4 Sidewinders |
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