Kuznetsov NK-144: Difference between revisions
Content deleted Content added
m updating link using AWB |
|||
| Line 13: | Line 13: | ||
{{reflist}} |
{{reflist}} |
||
{{ |
{{Aviation lists}} |
||
[[Category:Low-bypass turbofan engines]] |
[[Category:Low-bypass turbofan engines]] |
||
Revision as of 08:13, 5 July 2008
The Kuznetsov NK-144 is a afterburning turbofan engine used on the early models of the Tupolev Tu-144 supersonic aircraft. It is made by the Soviet Kuznetsov Design Bureau.
- Kuznetsov NK-144 user on: Tu-144/-144D/-144LL
- Thrust (kg): 28,660 (dry) 38,580 (wet)
- Airflow:551 lb/s
- OPR: 14.2
- BPR: 0.60
- Spools: 2 2
- SFC: 1.81 lb/lbf hour[1]
Data from:[2]