View attachment 757900
LOL! Yes they have switched to a 16 engine design! That's not what it originally looked like when your engineers proudly announced it years ago
So the original supa-dupa strap on boosters "bigger than the Space Shuttle's" envisioned/researched by your best rocket engineering minds has been ditched.
You can thank SpaceX for that.
Even with the removal of the 4 strap-on boosters, the new LM-9 will still be a very different beast compared to Super Heavy / Starship... this latest version is now actually more similar to the old Saturn V rocket..
Similarities to Saturn V :
- Stages : both are 3-Stage single stick heavy-lift rockets (no strap-on boosters)
- Propellant : both use dissimilar propellant between stages; 1st stage-Kerolox; 2nd & 3rd stage-Hydrolox.
- Appearance : both has dissimilar diameter between stages; 1st & 2nd stage same size; 3rd stage smaller.
- Reusability : Not reusable (but might change for LM-9 1st stage in the future)
- Flight profile : 1st & 2nd stage to get to LEO; 3rd stage for Trans-lunar injection
Differences to Saturn V :
- Engine : Number of engines clustering in 1st stage (5 vs 16) and 2nd stage (5 vs 4); for 3rd stage, both use only single engine.
- Payload to LEO : LM-9 is slightly more powerful (150T vs 140T)
- Saturn V is man-rated, while LM-9 is likely for cargo only
Otoh, between Starship and LM-9, the only thing even remotely similar is probably the large amount of engine clustering in the 1st stage... but even then, the number of engines is very different (30+ vs 16)... Other than that, everything else (number of stages, propellant, flight profile, etc) is totally different...
So I think it's totally wrong to claim the Chinese is copying Starship simply because they are now increasing the number of engines clustered in the core stage... even in its original form, LM-9 is already a rocket with clustered engines... 8 engines clustered in the core stage + 16 more engines distributed between the 4 boosters, for a total of 24 engines for the 1st stage... Right now they are just simplifying the design by removing the strap-on boosters and moving the booster engines to the core stage, while at the same time changing the engines with more powerful engines to
reduce the number of engines that needs to be clustered in the 1st stage (24 vs 16).
LM-9 original design
Also need to remember that the concept of clustering a large amount of small engines was actually first implemented by the USSR in their N-1 Rocket... 30 engines in the 1st stage... so no, it's not a monopoly of SpaceX nor is it a SpaceX original concept...
N-1 Rocket
Also, it's actually good that Chinese engineers are willing to review their designs and change it accordingly when something better comes along... rather than just forcing themselves to continue working on a dead-end design like NASA with SLS simply because they want to continue using legacy systems,..