Klimov RD-33
Encyclopedia
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Specifications
thrust=49.4 kN Dry, 81.4 - 88.4 kN Afterburning. http://i56.tinypic.com/2j2i82g.jpg
See also
External links
- Klimov official site page of RD-33 Turbofan engine family
- Official site page of RD-33MK
- Official site page of Thrust vector nozzle
- Official site page of SMR-95
- Official document: Prospective Project Developments 2007
- RD-93 for JF-17 / FC-1
- India to Build RD-33 under license
- India to make Mig 29 Engines with Russia
- RD-33 - history, versions, technical description (czech)
- RD-33 on Airwar.ru (russian)