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What’s most interesting about that (to me anyway...) is that they’re using a very imprecise machine (the telescoping forklift) to do what is traditionally a very precise operation (bolting space stuff together). Traditionally an operation like this would have a specific piece (or set) of GSE that would cost hundreds of thousands in capex, including hundreds of hours to design/fab...and the whole deal would be performed in a very controlled environment.
It might seem trivial, but this kind of approach is really where SpaceX sets itself apart from the rest of the industry.
What’s most interesting about that (to me anyway...) is that they’re using a very imprecise machine (the telescoping forklift) to do what is traditionally a very precise operation (bolting space stuff together). Traditionally an operation like this would have a specific piece (or set) of GSE that would cost hundreds of thousands in capex, including hundreds of hours to design/fab...and the whole deal would be performed in a very controlled environment.
It might seem trivial, but this kind of approach is really where SpaceX sets itself apart from the rest of the industry.
I had the same though regarding equipment. On the other hand, the engine attachment is via the positioning actuators and struts, so it is not a high precision operation like aligning two hard mount surfaces or installing a bearing.
Interesting. I would have just assumed the actuators and struts would have gone to a mounting plate, but it does make sense that you could just use them for the ‘precision’ part of the installation operation. Then any small misalignments could be calibrated out by some script that finds the new/real nominal zero point for the motor.
Those white struts are just transport equipment for securing the load in place, I also think that 'the black struts' are the actual actuators. (Electric ones I guess)
View attachment 414708
View attachment 414713
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Given the lack of space around the black struts, tight clevis, and lack of bends in the piping to the bell, I think the entire engine gimbals and those black struts are fixed.
That's a Falcon 1's thrust vectoring system. Falcon 9's TVC(s) are build lot tighter:
View attachment 414769
I read somewhere that: LOX line goes through the gimbal and methane (in) and tank pressurization (out) lines are (more) flexible:
View attachment 414770
Yeah, just watching those Merlin 1D pictures, is it hard to believe that there is enough clearance for movement. Also which pipes move with engine block and which flex in M1Dvac pic?
And there is lot more going on with Raptor and its test equipment...
Is it good idea lift it with forklift after all? (someone in NSF claims to see dent at SN4's bell, but who knows)