Does anyone have a chamber pressure trace for the original (SPM) SRM? It was used for STS-1 thru 7. Otherwise I'll have to take the HPM pressure trace and shift it in the same proportion as the thrust changed between the SPM and HPM, and hope the separation times +/- matches the real thing. :shrug:
As for the mass evolution, I got the numbers for the RSRM (so that is correct), and I've normalized the data to the max prop mass value, and will apply it to the other types (which will have different prop masses).
One other bit of info: I've added an extra data point at +/-21 seconds. This way our data doesn't "clip" the "corner" in plot of the real data where the initial thrust decay happens, which meant we had a (small) performance loss which now goes away.
---------- Post added at 04:32 PM ---------- Previous post was at 04:17 PM ----------
One question for the graphics department: is there any issue that could come if the pads and/or MLP meshes were rotated to some other orientation? I'm asking because currently when the vehicle sits on the pad it says it is horizontal instead of vertical, and I think that comes from it being attached to the ground vessels which are landed "horizontally".
I'll take a look at this only after I finish the SRM nightmare, but I wanted to get the ball rolling on this one.