D-20 by Soloviev
First Soviet twin-spool bypass turbojet (turbofan) engine.
| Model |
D-20 |
|
| Year |
1959?
|
| Type |
bypass turbojet |
| Takeoff |
| Thrust |
5400kg |
| Fuel consumption |
?kg/kgf/hour |
| Cruise |
| Thrust |
1100kg |
| Fuel consumption |
0.9kg/kgf/hour |
| other parameters |
| Bypass ratio |
? |
| Compression |
? |
| Maximum turbine inlet temperature |
°K |
| Resource |
?h |
| Length |
?mm |
| Maximum Diameter |
?mm |
| Weight |
?kg |
|