I've fixed the pushbutton issue (it's a bug in PushButton.cpp). Should I check the fix in to the trunk, or do you need in the MPS branch?
I've fixed the pushbutton issue (it's a bug in PushButton.cpp). Should I check the fix in to the trunk, or do you need in the MPS branch?

2.92116, -3.44059, -10.8442

LO2, on the starboard sidewall of the aft compartment. The other two "panels" are the 9(FWD) and 8(aft) vents.Yep, that's the middle of the 3 panels that I mentioned above, so looks like it's that "dot".
Those coordinates are of what vent, LH2 or LO2? (need both)
Don't worry about pictures, I just need the coordinates.![]()
-0.434188, 1.5138, -10.8137
LO2, on the starboard sidewall of the aft compartment. The other two "panels" are the 9(FWD) and 8(aft) vents.
LH2 feedline relief pos:
Try this if you don't already have them: https://web.archive.org/web/20050720004209/http://spaceflight.nasa.gov/shuttle/reference/sodb/Code:-0.434188, 1.5138, -10.8137
Could you describe the problems you're having with the C3 switches? Do they physically need to change in the actual VC or is it code?I have those for some years now, thanks anyway. And thanks again for the coordinates. :thumbup:
If you have time please correct the positions of the switches in panel C3.
So code then. Try these:I think the coordinates are not exactly correct, because the switches are kind of "floating" above the panel.... it's a similar issue to what we had in some switches in panel R2 sometime ago.
ET sep: -0.08218, 1.69955, 14.06513
SRB sep: 0.00608, 1.70746, 14.0791
This could explain things. I just completed an ascent of STS-61G with the max SSME throttle set to 104% instead of the planned 109%. I did hit the target MECO parameters but only with 18 tons of propellant left in the ET. I did add the MPS manifold propellant mass (5400 lbs).Just was thinking about changing the way the ET and MPS interact (to be able to do ullage pressures and level sensors), and I might have found (another) cause for the excessive performance during ascent: in reality there is propellant both in the ET and in the MPS manifold, but I'm not sure if in our ET propellant mass we are including the ~5400lbs from the manifold.
Another possible thing is that some of the propellant that comes into the orbiter gets vaporized and sent back to the ET to keep ullage pressure up. That tiny amount of mass, over 8.5mins, could make a difference...

I switched branches to test the MPS implementation so far and everything works very nicely. Just one question though: is the MPS GH2 INERTING procedure implemented? If so, how do I access panel R4?
We do have panel R4 as well L4 on the CDR side. Here's a screenshot of R4:Currently only the MPS dump and both vacuum inerts are done, all auto (I remember to be missing one part somewhere, maybe that's what you're referring to).
That's probably going to be done (plus the reentry purge/press/whatever) after I do the "ET/MPS mods". But I also need panel R4, which currently doesn't exist, and even if existed the current "head position" doesn't allow proper viewing of it.