Very simply, FT9's maximum payload capacity is designed based on the optimal dimensions for a 3.7-meter diameter 2-stage rocket.Does CZ-10B use methane as fuel? It's much larger than a Falcon 9 FT B5 (3.66m diameter, 69.8m tall) yet payload is alot less (18.5t for downrange recovery vs 16t).
CZ10B has a larger diameter. However, its height is slightly smaller than FT9. This indicates its aspect ratio has not been fully utilized.
CZ10's aspect ratio can reach the level of FT9, which means a maximum height > 90m (currently it is a 3-stage configuration)
While CZ10B's maximum height is less than 70m. Therefore, CZ10B's current configuration is not its true optimal solution.
Secondly, there is the total thrust of the first-stage engines. This total thrust is not much greater than the first-stage total thrust of the Falcon 9.
However, the 5-meter vehicle body is significantly larger and much heavier than the 3.7-meter vehicle body, and considering the second stage of the CZ10 series is also actually on the smaller side
So it is normal that the payload capacity is a bit lower. Achieving 16t with first-stage recovery is already sufficient.
The design of CZ10 is an optimal design centered on a CBC configuration 3-stage rocket. The single-stick 2-stage configuration cannot possibly be the optimal design




