Engine developed for the Neutron vehicle.
Mass (kg)
not publicly available
| Specification | Value |
|---|---|
| Mass (kg) | not publicly available |
| Gimbal (deg) | not publicly available |
| Propellants | Liquid Oxygen (LOX) / Methane (CH4) |
| Vacuum ISP (s) | 365 367 |
| Mixture Ratio | not publicly available |
| Restart Count | not publicly available |
| Vacuum Thrust (N) | 890000 |
| Sea-Level Thrust (N) | 730000 |
| Chamber Pressure (bar) | not publicly available |