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Purpose:
Turbofan aero engine
Description:
Designed to power the An-124, An-124-100 Ruslan and
An-225 Mriya ramp-equipped heavy transport aircraft.
The engine design allows to operate it on technical condition
up to serving out the service life of main parts. The
engine has Type Certificate. It meets the effective environmental
requirements of ICAO standards.
Technical details:
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Takeoff (SLS; ISA):
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thrust, kgf
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23430
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specific fuel consumption, kg/h/kgf
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0.345
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Max cruise (H11 000 m,M 0.75; ISA):
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thrust, kgf
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5000
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specific fuel consumption, kg/h/kgf
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0.561
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Dimensions, mm
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5 400х2 937х2 792
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Weight, dry, kg
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4100
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Operating life, h (cycles)
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24
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