First-stage LOX/kerosene rocket engine of the Soviet N1 Moon rocket, predecessor to NK-33 with 1,510 kN sea-level thrust.
NK-15 Rocket Engine
First-stage LOX/kerosene rocket engine of the Soviet N1 Moon rocket, predecessor to NK-33 with 1,510 kN sea-level thrust.
Description
The NK-15 was the first-stage rocket engine of the Soviet N1 Moon rocket, burning LOX and kerosene in an oxygen-rich staged combustion cycle. The N1 first stage used 30 NK-15 engines in clustered configuration. The NK-15 was later refined and improved into the NK-33, which achieved significantly better performance and reliability.
Specifications
| Propellants | LOX / RP-1 (kerosene) |
|---|---|
| Cycle | Oxygen-rich staged combustion |
| Thrust (sea level) | 1,510 kN |
| Application | Soviet N1 Moon rocket, first stage |