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Basic characteristics Su-26 Su-29 Su-31 Su-31M Su-26M3
Production year 1988 1991 1992 1995 2003
Basic dimensions:
- wingspan, m
- length, m
- height, m
- wing area, m?

7.80
6.827
2.40
11.83

8.20
7.29
2.885
12.20

7.80
6.83
2.76
11.83

8.20
6.883
2.76
12.17

8.20
6.867
2.749
12.17
Engine,
Rating, hp
M-14P
360
M-14P
360
M-14PF
400
M-14PF
400
M-9F
420
Maximum takeoff weight, kg 962 1,220 1,050 1,100 1,100
Training mode takeoff weight with full integral tankage, kg 850 1,027 858 909 890
Aerobatic mode takeoff weight, kg 790 884 805 866 857
Dead weight, kg 700 790 700 760 750
Maximum fuel, kg 143 202 215 215 206
Maximum permissible flight speed, km/h 450 440 450 450
Maximum horizontal flight speed, km/h 310 325 330 330 340
Landing speed, km/h 120 115 115 130
Rate-of-climb, m/sec 18 16 24 24 21.5
G-limit (operational) +12 / -10 +12 / -10 +12 / -10 +12 / -10 +12 / -10
Roll rate, rad/sec 5-6 6 7 7 7
Flight range, km 895 1,200 1,100 1,100 1,200
Takeoff / landing run (normal takeoff weight), m 120 / 380 110 / 300
Survival systems parachute
PNL-60
parachute
PNL-91
parachute
PNL-91
system
SKS-94
system
SKS-94M


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