That actually has a bit more power than the RD-180. 5 MN. This is supposed to be for which rocket? Not the lunar one I think.
The chamber pressure is a lot higher than previous Chinese rocket engines at 22.0 MPa vs the RD-180s 26.7 MPa. YF-100 was just 18 MPa.
A single such rocket engine could probably power an entire LM-7 rocket first stage. It would bring manufacture costs for medium lift launch vehicles way down.
The chamber pressure is a lot higher than previous Chinese rocket engines at 22.0 MPa vs the RD-180s 26.7 MPa. YF-100 was just 18 MPa.
A single such rocket engine could probably power an entire LM-7 rocket first stage. It would bring manufacture costs for medium lift launch vehicles way down.
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