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Dual-Flow Turbojet Engine RD-33 for Aviation Applications

Turbojet Engines

Manufacturer:MMP named after V.V. Chernyshev OJSC

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Description

Two-circuit, twin-shaft, turbojet with flow mixing in a common afterburner and vane jet nozzle

Specifications

Diameter

1040 mm

Assignment

for installation on all modifications of the world-famous, combat-proven MiG-29 fighter aircraft

Degree of dual circuit

0.49

Length

4229.5 mm

Weight

1055 kg

Overhaul life

800

Assigned resource

1600

Designation

RD-33

Total degree of pressure rise

Specific fuel consumption at full boost mode, kg/kg/h

2.05

Air flow rate, kg/s

Thrust at max. mode without afterburner, kgf

5040

Thrust at full force mode, kgf

8300

Specific fuel consumption at max. mode without afterburner, kg/kg/h

0.77

Note: All specifications are provided by the manufacturer and may be subject to change. Please contact us to confirm the latest specifications before placing your order.

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Shipping Terms

FOB Novorossiysk, RussiaCIF Available to major ports worldwideEXW Manufacturer's facility, Russia

Delivery Time

Sea freight: 30-60 days (depending on destination) Air freight: 14-21 days (for urgent orders)

Payment Methods

Letter of Credit (L/C)Wire Transfer (T/T)Escrow Services

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Dual-Flow Turbojet Engine RD-33 for Aviation Applications

Description

Specifications

Share your requirements for a quick response!