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P.S. just for clarification, Falcon Heavy (LEO 63,8 tonne stated) is way more heavier than LM5 (25t LEO), a different category together with China's 921 rocket at 70 tonne LEO.
Totally different. You can't compare Long March 9, a rocket with 10m diameter, with Falcon Heavy which uses three rockets of 3.66m diameter. Logistics, logistics, logistics. SpaceX can just bring the Falcon Heavy rocket parts by road on the flatbed of a truck, while LM9 requires a barge to bring it to the launch site. Plus it requires completely different facilities like I said before.
I compare both rockets, yes, because Falcon Heavy so far has mostly been launched in reusable mode.
Which won't give you 63.8tons. Expect half that.
Falcon Heavy originally was meant to compete with the Delta 4 Heavy for DoD and NRO payloads.
As Falcon 9 basic booster performance went up with Merlin engine upgrades and stage stretches the numbers went up quite a bit. But it was originally meant to compete with a rocket like Delta 4 Heavy, Ariane 5, or LM5. LM9 is supposed to launch 140ton to LEO which makes it in the launch category of SLS. i.e. mostly useless.
Just consider this. The smallest LM9 configuration has more than thrice the performance of the largest satellites like Hubble. How many launches of Hubble sized payloads do you think you will see over the next decade? Let alone LM9 sized ones. Why do you think Ariane 5 does dual launches despite being much smaller? Have you ever looked at a chart of satellite masses? They are going down on average ever since satellites switched from chemical to ion propulsion. The average GTO satellite is like 4ton. Zarya is probably one of the largest ISS modules and it's just shy of 20ton (LEO). You can launch that in LM5. You could also launch Hubble with LM5.
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