RD-0120
| Use attributes for filter ! | |
| Nozzle ratio | 85. 70 |
|---|---|
| Thrust-to-weight ratio | thrust |
| Manufacturers | Voronezh Mechanical Plant |
| Propellant | LOX |
| LH2 | |
| Chamber pressure | 21. 9 MPa (3,180 psi) |
| Thrust (vac.) | 1,961. 3 kN (440,900 lbf) (106%) |
| Date of Reg. | |
| Date of Upd. | |
| ID | 2981095 |
About RD-0120
The Soviet RD-0120 was the Energia core rocket engine, fueled by LH2/LOX, roughly equivalent to the Space Shuttle Main Engine. These were attached to the Energia core rather than the orbiter, so were not recoverable after a flight, but created a more modular design.