Kuznetsov NK-144
From Infogalactic: the planetary knowledge core
| NK-144 | |
|---|---|
| Type | Turbofan |
| National origin | Soviet Union |
| Manufacturer | Kuznetsov Design Bureau |
| Major applications | Tupolev Tu-144 |
The Kuznetsov NK-144 is an afterburning turbofan engine made by the Soviet Kuznetsov Design Bureau. Used on the early models of the Tupolev Tu-144 supersonic aircraft, it was very inefficient and was replaced with the Kolesov RD-36-51 turbojet engine.
Specifications (NK-144)
- Data from:[1]
- Thrust (kg): 28,660 (dry) 38,580 (wet)
- Airflow:551 lb/s
- Overall pressure ratio: 14.2
- Bypass ratio: 0.60
- Spools: 2 2
- Specific fuel consumption: 1.81 lb/lbf hour[2]
References
External links
- NK-144 on LeteckeMotory.cz (Czech)
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