I think we should view the CZ-9 and the production complex project somewhat separately.
On the question of "project approval", it's a bit opaque to outsiders but I think it's generally analogous to the development process in the Chinese MIC sector for engines and weapon systems (pre-research stage, formal R&D stage, etc.) with formal project approval usually being granted or denied only after years (or decades) of work and the existence of substantial work-product. But I think the CZ-9 project is definitely nearing realization given that land for the VAB and associated buildings are being acquired and initial prep work is being done (and the fact that the local government is publicly talking about it). I'll just quote TheRatholos post #8,028 from Arpil of this year:
The reference to the CZ-9 being explicitly mentioned by sci/tech representatives as one of the goals during the 15th Five-Year-Plan is from the following link (also posted in this thread from back in April):
The 2030 date for the first flight of CZ-9 was mentioned in various PPT slides, see attached image from 2025(?). The version they want to launch by 2030 is likely the base CZ-9 with a reusable 1st stage; CZ-9B is the fully reusable version planned for later (around 2033). The variant with a Starship-like upper stage which has been displayed in model-form at shows may also be called CZ-9B (9BG ?) or may something else, and the same goes for the variants with three stages and 16 metre fairings. What's clear is that variants within the CZ-9 family is likely to pop up like mushrooms much like with all the other new generation Long March families. Possible uses for the CZ-9 family that have been mentioned by various people in the Chinese space sector include: delivery of lunar surface and martian surface infrastructure, construction of Mars-bound crewed spacecrafts, experimental solar power stations etc. They'll probably come up with additional possible uses (eventually, we may be talking about scenarios envisioned by 2001: A Space Odyssey and by Gerard O'Neill back in the 1960's and 1970's ... one can hope right?)
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In the medium term, the ability to execute on this will of course be rate limited by YF-215's progress as well (and also launch/fueling/production infrastructure overall), but a wildcard in terms of future variants may be the in house engineering and development teams. If they really put out CZ-12B in under 2 years from first design work to first launch, then the future state capability might be a lot more dynamic than we project, if bottlenecks can be resolved.
the timeline quoted by different CNSA/CATL members is early 2030's not 2030..If I recall correctly (kinda big if, I haven't followed CN space scene closely at all. It's possible I'm misquoting)
Cute Orca (whom I consider even more reliable wrt CN space watching than PLA watching) has basically scuffed at the CZ-9 2030 launch date. He thinks the overall project isn't even close to being on track for that target
If I recall correctly (kinda big if, I haven't followed CN space scene closely at all. It's possible I'm misquoting)
Cute Orca (whom I consider even more reliable wrt CN space watching than PLA watching) has basically scuffed at the CZ-9 2030 launch date. He thinks the overall project isn't even close to being on track for that target
AFAIK, these drawing (Except for the first one) are highly speculative and does not match any known official designs. It is doubtful whether any near future variants will look like this.A few more depictions, derived from Echo5550's art on twitter.
In any case, the 15-16m fairing variant would likely be a later variant to grow into.
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This one by 卡尔达瓦里希
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AFAIK, these drawing (Except for the first one) are highly speculative and does not match any known official designs. It is doubtful whether any near future variants will look like this.View attachment 176268
Officially CZ-9 with standard fairing is only 110m tall while the reusable CZ-9B is 95m. The booster itself from the looks may only be 45-50m tall. The latter two of the drawing shows a design with stretched boosters which is IMO unlikely in the near future given the initial CZ-9 design with YF215s can achieve a TWR at takeoff of 1.4 but any major stretch like the ones depicted would require far more powerful engines for it to be efficient.