Some thoughts on CZ-12B, recent medium lifters, and other PRC rocket engines and the future.
CZ-12B is said to have started development in September 2024 with its design approved in March 2025, and even though it is a somewhat conservative kerolox design, the speed of its emergence, and using relatively new engines (YF-102 is somewhat recent even if it's not cutting edge SOTA), and in a relatively mature fitout including landing legs and gridfins, and all in a clean sheet rocket fuselage/diameter (different to CZ-12, CZ-12A), does point to a fair bit of design and industrial capacity that exists if other bottlenecks can be met.
With various other reusable medium lifters flying or due to fly (and if even only a fraction of them achieve high cadence launch/recovery), that will likely prove a solid foundation for the next step of progressing to proliferation of heavy and even super heavy lifters.
Needless to say methalox FFSC engines are the future, and afaik there are three major efforts ongoing at the moment, all in the 200t+ thrust class
- YF-215, by CASC, also the intended engine for CZ-9's first stage that has been seen pretty consistently for last couple of years. While CZ-9 is intended to fly post 2030, the engine itself may be a different matter. 200t+ class
- BF-20, by landspace, and landspace have indicated a desire to develop a super heavy of their own using BF-20 circa 2030, 220t
- FY-200V, by JZJY (who have developed LY-70 that is used on CZ-12A), which is a 300t class engine
Which are three methalox FFSC in the 200t+ class by pretty credible entities (not including a couple others by startups lacking in detail or record).
What this means, is that CZ-9 probably isn't the only heavy/super-heavy to expect in the next half decade or so (even if one considers its status as "not fully funded" which in PRC space parlance can mean lots of things), and we can probably expect the various 200t+ methalox FFSC engines being developed to end up having applications on other rockets that could emerge somewhat briskly without excess leadup time in the way CZ-12B did.
For example we know CASC has looked at a 7m, reusable 50t LEO rocket powered by 13x methalox FFSC engines in the 200t class (likely YF-215), in addition to a 10m, reusable 100t LEO rocket powered by 30x such engines (basically CZ-9, if not directly CZ-9) itself.
(Picture at bottom)
So overall, I wouldn't be too surprised if a handful of heavy or even super heavy rockets emerge on a faster "turn around time" than CZ-9 in future, in terms of "public being aware of its consideration/initial investigations --> first launch"... and it will be entirely depend on the "commoditization" of the upcoming generation of methalox engines.
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