Thanks my friends for liking my work.

Hello everybody,
after the two
ET/Orbiter Assemblies are now finally completed, there is always still a small line missing, and this is the so-called
LH2 Recirculation Line (Ø 4''), which can be seen here on the
ET-45 (STS-47).

Source: georgesrockets.com (George Gassaway)The line looks relatively simple and has a slight kink at both ends,
Source: forum.nasaspaceflight.com (DaveS)
Source: System Definition Handbook SLWT, Vol. II (Lockheed Martin)in front of each time a
Protective Shroud sits.
Source: System Definition Handbook SLWT, Vol. I (Lockheed Martin)And so plain and simple looks this part of the
Airfix Kit, whereby the two
Shrouds are missing, which is not the end of the world.


First, I've tried it again with a
Copper dummy (Ø 0,6 mm), and then I've tried to drill out a
Rod ( Ø 1,2 mm) for the
Shrouds stepwise in the center up to
Ø 0,7 mm, which is not that easy with this diameter.

After the temporary installation of the Dummy, which did not cause any problems,


I've then bent an
Evergreen rod (Ø 0,7 mm) for the final line.
As already mentioned, drilling out can not be made immediately to the final inner diameter (Ø 0,7 mm), because the drill can slip too easily and does not stay in the center, therefore carefully step by step.


After that, I've cut off small 0,5 mm wide rings and had to find out that the bore had run eccentrically inwards, so unfortunately only the front ring could be used.



That's why I then drilled out only still 1 to 2 millimeters and then cut off the ring so as not to produce too much rejects.


And that's how I actually managed to make three useable rings,

and to thread them onto the rod, whereby the line looks significantly better than the Airfix cripple.


But when I kept the result of the test fitting in my sight,

I was a little disenchanted, because the line seemed a bit too puny compared to the
LH2 Feedline,


what I've remembered differently when seeing all the photos ...

Source: NASAAnd when I was brooding about it,

suddenly it felled from my eyes like scales ...
Out of power of habit of recent weeks in intensive dealing with the
GH2/GO2 Press. Lines, whose diameter is
2" (Ø 0,4 mm/1:144) and which are "naked", i.e. have
no TPS cladding, the diameter of the
LH2 Recirculation Line of
4'' (Ø 0,7 mm), which was used by me as a reference measure, concerns also only the "naked" stainless steel line, but which still has a
1'' TPS cladding (SS-1171/SLA-561), what results in a diameter of
6'' (Ø 1,0 mm/1:144), what I should have taken into account (see right scaling),

Source: georgesrockets.com (George Gassaway)which is why I've then used the corrected dimensions.

Source: capcomespace.netFor the new line with the larger diameter
(Ø 1,0 mm) I have then punched small discs
(Ø 1,5 mm) for the
Shrouds with my
Punch & Die Set made of
Styrene (1,0 mm) ,

which I've then drilled out in nine steps from
Ø 0,5 mm to
Ø 1,0 mm and chamfered,

and then threaded onto the new bended line that I like much better now.


Then I've drilled out the openings in the
Umbilcal Plate as well as in the
ET Aft Dome to 1 mm and carefully inserted the line, which now fits much better into the mould,

as one can clearly see here in the comparison of both variants.


Just good thing I've still noticed this lapse and could correct it,


because with it now I can finally finish this
Umbilical chapter.


Now only a small detail is missing on the
Crossbeam, which still has this cover with the outer slight slants on the top at the front edge, what it also was always good for ...

Source: NASAThis last detail I also still want to scratch now, wherewith then the
ET/Orbiter Aft Attachment would be complete in my eyes.
