The 1S17 version of the SaM146, which powers the baseline SSJ100, develops 17,300 lbs of thrust. Entering revenue service in 2011, the SaM146 has posted exceptional dispatch reliability (99.9%), along with adaptability to all operating environments, whether hot or cold.
TECHNICAL CHARACTERISTICS
Application
Sukhoi Superjet 100
Takeoff thrust (lbf)
15,400
Bypass ratio
4.43
Max. climb thrust (lbf)
3,740
Fan diameter (in)
48.2
Length (in)
141.34
Dry weight (lbs)
4,980
The 1S17 version of the SaM146, which powers the baseline SSJ100, develops 17,300 lbs of thrust. Entering revenue service in 2011, the SaM146 has posted exceptional dispatch reliability (99.9%), along with adaptability to all operating environments, whether hot or cold.
| TECHNICAL CHARACTERISTICS |
|---|
|
|---|
| Application | Sukhoi Superjet 100 |
| Takeoff thrust (lbf) | 15,400 |
| Bypass ratio | 4.43 |
| Max. climb thrust (lbf) | 3,740 |
| Fan diameter (in) | 48.2 |
| Length (in) | 141.34 |
| Dry weight (lbs) | 4,980 |
