The LM8 configuration faces no major issues in modifying for reusable rockets. The CZ-6X solution demonstrates this. You need to assess technical feasibility through engineering principles. Reusable rockets don’t require engines to adopt concentric circular layouts. The core requirement is achieving a thrust ratio (maximum liftoff thrust to minimum throttled thrust) around 20:1 or higher—a value fundamentally dictated by Earth’s gravity well. This ratio also explains why launch vehicles’ maximum payload mass fraction barely reaches 5%. The LM8’s hybrid engine configuration (combining large and small thrusters) could achieve this target.They had a plan to make the LM8 reusable, but it was a pipe dream. The LM-8 is not designed to be reusable. The original plan was for the LM8 to land with it's boosters attached. Never gonna happen, it's as ridiculous as the Vulcan's plan to drop it's rocket engines from orbit encased in a heat shield for reuse. Just a desperate plan to make an already obsolete rocket seem more attractive in the age of reusable rockets. For reusable rockets, all of them have a few things in common, that is their engine layout. A central engine surrounded by a ring of even numbered engines.
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This is to balance out the thrust, so as to ensure that the rocket doesn't get unbalanced. Also, reusable rockets use a larger number of weaker engines that can be throttled, instead of the old style of a handful of extremely powerful engines. But the core layout is still the most important factor here.
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None of China's current LM rocket fleet fit this criteria, even if their engines are designed for reuse and throttling. The LM-8 has a 2 engine layout and optional boosters, the LM-12 has a 4 engine layout. And of course you can't just change the engine layout of a rocket willy nilly, especially not adding new engines in. Making the LM8 reusable is like trying to make a brand new rocket. That's basically what's happening to the LM-12, another waste of money. Despite being the last in development of the LM family, they didn't get the memo that reusable rockets were the new hottest until the original expendable design was already completed. SAST developing a reusable version of the LM12 is like developing a new rocket from scratch and thus developing two different rockets, they would have been better if they done what the CZ-9 team did and pivoted mid-design phase to save money and time, and not finished the expendable design at all.
If the LM-8 is already obsolete, then I wonder how many times the expendable LM-12 will be flying? Probably less than 5 times over it's entire lifetime I bet.
In fact, the old LM9 reusable concept followed similar logic.
The reason LM8 won’t develop a reusable version lies in its insufficient post-reusability payload capacity (inherently limited by low baseline liftoff mass). To increase payload while controlling landing mass, a single-core, 3.8-meter-diameter design becomes mandatory.
Observe Falcon 9’s evolution: the drastic differences between v0.9 and v1.2 highlight how expendable-optimized designs must be radically scaled up for reusability.
The LM12 itself has three designs, including two reusable variants (see: ).
Reusable rocket development—like all complex engineering—follows phased iterations. First, stabilize baseline functionality (perfecting expendable operations), then attempt reusability. Falcon 9 required ~30 launches to achieve reliable reuse.