| General |
|
| Design
organisation |
Sukhoi
Design Office |
| Main
secundary design organisations |
Motor
Building Association and NPO Saturn Research and Production Association |
| Production
organisaton |
- Komsomolsk-on-Amur
Aviation Production Association (KnAAPO) |
| Primary
task |
Multi-role
fighter jet |
| Type
aircraft |
4++
generation fighter jet |
| Specials |
|
| Length |
21.9
meters |
| Height |
5.9
meters |
| Wingspan |
15.3
meters |
| Wing
surface |
|
| Aspect
ratio |
|
| Sweep
back |
|
| Dihedral |
|
| Performance |
|
| Engines |
2x 117S
turbofan with afterburner and Trust Vector Control |
| Thrust |
8.800
kgf
14.5000 kgf (with afterburner) |
| Weight
(empty) |
25.3000
kgs |
| Weight
(start, maximum, MTOW) |
34.500
kg s |
| Weight
(landing, maximum, MLW) |
|
| Required
runway length (start) |
|
| Required
runway length (landing) |
|
| Cruise
speed |
|
| Maximum
speed |
1400
km/h (MSL)
2400 km/h (high altitude)
Mach 2.25 |
| Ceiling |
18.000
meters |
| Maximum
range |
1580
km (MSL)
3500 km (high altitude)
1500 km (+ 2 external fuel tanks) |
| Fuel
capacity |
11.500
kgs |
| Air-to-air-refueling
capability |
Yes |
| Passengers |
none |
| Payload |
none |
| Equipment |
|
| Armament |
30mm
boardcanon
Air-to-air missiles
Air-to-ground missiles |
| Maximum
weapon load |
8000
kilograms over 12 pylons |
| Maximum
G resistance |
+9 |
| Radar |
Irbis-E,
passive phased, antenna |
| Sensors |
|
| Avionics |
|
| Type
flight controls |
|
| Landing
gear |
|
| Usage |
|
| Versions |
Su-35BM |
| Manufactured |
|
| Crew |
1 or
2 |
| Costs |
|
| Overall
flight hours |
6000
hours |
| First
flight |
19 February
2008 |
| First
delivery |
n.a |
| Operational
since |
n.a |
| Successor
of |
Su-30MK |
| Replaced
by |
n.a. |
| Comparable
aircraft |
Eurofighter
Typhoon, Rafale |
| Operators
(current and future) |
none |
| Main
operators |
none |
| Amphibious
usage |
No |
| Status |
In development |
