NK-144
Development of NK-8 engine, modified for supersonic operation.
Other design details:
| Model |
NK-144 |
NK-144A |
Tu-144 prototype
Tu-144S
|
| Year |
? |
? |
| Type |
bypass turbojet |
bypass turbojet |
| Full Afterburner |
| Thrust |
17,500kg |
18,150kg |
| Fuel consumption |
?kg/kgf/hour |
?kg/kgf/hour |
| Maximum without afterburner |
| Thrust |
13,000kg |
15,000kg |
| Fuel consumption |
?kg/kgf/hour |
?kg/kgf/hour |
| other parameters |
| Bypass ratio | ? |
| Compression | ? |
| Maximum turbine inlet temperature |
?°K |
| Resource |
?h |
| Length |
5200mm |
| Maximum Diameter |
1500mm |
| Weight |
?kg |
...
|
