D-18T
Engine · Ukraine
Original archive entry. The text, images and links below are kept as they were written.
Lotarev turbofan engine. Used on An-225 launch aircraft for Interim HOTOL, MAKS concepts. Development ended 1988.
Thrust (sl): 203.900 kN (45,839 lbf). Thrust (sl): 20,796 kgf. Engine: 4,500 kg (9,900 lb). Thrust to Weight Ratio: 5.19.
Related
- Family
- Turbofan
- Country
- Ukraine
- Launch Vehicles
- MAKS, Interim HOTOL
- Propellants
- Air/Kerosene
- Agency
- Lotarev
- Bibliography
- 303