RD-33 ENGINE

General Description
Product Specifications
Gallery & Media
Point of Contact for further follow up
Others
Product Manufacturer
Hindustan Aeronautics Limited (HAL)
Product Description

 Twin spool turbofan engine with 4 & 9 stage LP & HP compressor respectively
and 2 stage turbine powering MiG-29 aircraft.
Platform: MiG-29 fighter aircraft

Product Specification
Basic Information
Compressor Ratio - 20-22
Air Mass Flow (Kg / Sec.) - 76+1.5
Thrust (KgF) - Max Dry / AB 5040 / 8300
By Pass Ratio - 0.45
Specific Fuel Consumption - 0.77-2.05
TBO / TTL (Hrs) - 350 / 1200
Contact : prasenjit[at]hal-india[dot]co[dot]in