Is this engine the same one that will be used on the new manned spacecraft service module (where they will be four engines)?The 7500N variable thrust engine used for landing Chang'e 3, 4, and 5 landers on the moon.
Trust me, we are much more shrewd this time around. Galileo ended up like that because the Chinese leadership and elites back then believed in the whole "Western World honors the spirit of the contract", "Western leader are held accountable by their political systems", and other public intellectual (公知) bullshit. Now, we look at these as a joke.
Sounds to me like a rehash of the old Galileo GNSS strategy to me.
And @by78,Is this engine the same one that will be used on the new manned spacecraft service module (where they will be four engines)?
And @by78,
The answer is no. The manned landing module need 8t class deep throttling engine (10:1). 7500N X 4 = 3t, not powerful enough, it is also limited to 5:1 throttling, not deep enough. Note, the actual range is 6.87:1.
There is at least a study since 2016 about 8t (10:1) engine which is Kerosene/LOX closed cycle draw experience from the work of YF-100 (65% throttling).
For comparison, the Apollo decent engine LMDE is 4.5t 10:1. So the Chinese manned lander is twice the mass of Apollo program.