Progress D-18T

Length

5400 mm

Dry Weight

4100 kg

Thrust To Weight

5.72

Architecture

Fan	Fan Stages —	Fan Blades —	Fan Technology —	Fan Pressure Ratio —
Gearbox	Geared Fan No	Gear —	Reduction Ratio —
LP compressor	Low-Pressure Compressor Stages —	Low-Pressure Compressor Technology —	BP Compressor Pressure Ratio —
IP compressor	Intermediary-Pressure Compressor Stages —	Intermediary-Pressure Compressor Technology —	IP Compressor Pressure Ratio —
HP compressor	High-Pressure Compressor Stages —	High-Pressure Compressor Technology —	HP Compressor Pressure Ratio —
Combustor	Combustion Chamber Annular combustion system
HP turbine	High Pressure Compressor Stages —	High-Pressure Turbine Technology —
IP turbine	Intermediary-Pressure Turbine Stages —	Intermediary-Pressure Turbine Technology —
LP turbine	Low-Pressure Turbine Stages —	Low-Pressure Turbine Technology —
Whole engine	Streams 2	Bypass Ratio —	Overall Pressure Ratio —	Afterburner No

No pictures yet for this family.

Name	Aircraft Engine	Number of Engines	Length (m)	Flat Wing Span (m)	Max Seating
Antonov An-124 Ruslan	Progress D-18T	4	69.1	73.3	88
Antonov An-225 Mriya	Progress D-18T	6	84	88.4

All data (13 fields)

Name: Progress D-18T
Aircraft Engine Manufacturer: Ivchenko-Progress ZMKB
Aircraft Engine Type: Turbofan
Dry Weight (kg): 4100
Length (mm): 5400
Wikipedia Article (URL): en.wikipedia.org/wiki/Progress_D-18T
Geared Fan: No
Combustion Chamber: Annular combustion system
Afterburner: No
Streams: 2
Thrust To Weight: 5.72
Compressor Description: Single-stage fan, seven-stage IP compressor, seven-stage HP axial compressor
Turbine Description: Single-stage HP turbine, single-stage IP turbine, four‑stage LP turbine