Kuznetsov NK-144
Jump to navigation
Jump to search
| NK-144 | |
|---|---|
| Script error: No such module "InfoboxImage". | |
| NK-144 engine on a pedestal near the building of KAI in Kazan. | |
| Type | Turbofan |
| National origin | Soviet Union |
| Manufacturer | Kuznetsov Design Bureau |
| First run | July 1964 |
| Major applications | Tupolev Tu-144 |
| Developed into | NK-22 |
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
Data from [1]
General characteristics
- Type: Twin-spool afterburning turbofan
- Length:
- Diameter:
- Dry weight:
Components
- Compressor: axial
Performance
- Maximum thrust: 28,660 lbf (dry) 38,580 lbf (wet)
- (127.40 kN 63,185 lbf to 171.2 kN
- Overall pressure ratio: 14.2
- Bypass ratio: 0.60
- Air mass flow: 551 lb/s
- Specific fuel consumption: 1.81 lb/lbf hour[2]
References
<templatestyles src="Reflist/styles.css" />
Script error: No such module "Check for unknown parameters".
External links
Script error: No such module "Side box".
- NK-144 on LeteckeMotory.cz (Czech)
Script error: No such module "Navbox".
| File:Aero-stub img.svg | This aircraft engine article is missing some (or all) of its specifications. If you have a source, you can help Wikipedia by adding them. |
