CHERNYSHEV MOSCOW MACHINE-BUILDING ENTERPRISE

RD-93


 




 

 

 Thrust at full reheat rating

 8300kgf

 Maximum dry thrust

 5040kgf

 SFC at full augmented rating

 2.05 kg/kg h

 SFC at max. dry thrust

 0.77 kg/kg h

 Air flow

 76±1,5 kg/s

 Bypass ratio

 0,49

 Overall pressure ratio

 21±1

 Length

 4230 mm

 Diameter

 1040 mm

 Dry weight

 1055 kg

 Total technical life

 1200 h

 TBO

 600 h


At present there are developed several modifications of the engine with low location of the engine accessory drive gear box (RD-33N, RD-93, SMR-95) for single engine fighters including MiG-21, Mirage III, Mirage F-1 etc.

The SMR-95 engine has passed successfully flight tests on fighters Super Cheetah D-2 of the UAR Air Force. As a result of installation on them the SMR-95 engine (thrust at full reheat is increased by 16 %, SFC is decreased by 25 %) flight performance and efficiency of aircraft in combat increased 1.2-3 times.







PRESENTATION OF THE COMPANY 
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