Indeed for the xml.
Like in real , I guess we can adjust the nominal one following the profile will fly , like a I load mission specific
I just changed the max to 109 ( 106 before ) and abort to 106 ( 109 ) before .
It was flipped .
For the performance issue , i have good documentation’s With propellant remaining , etc
Need to find it now
For me 6 pour-cent seems legit .
A ful’ Eastward with no payload .
Shuttle would have been able for polar orbit and heavy payload .
So I guess there was margin for a full earth relative speed assistance launching due east compared to what was forecasted for polar orbit.
I am wondering , because empty but with the 40000 pounds equipment was like fully loaded orbiter for your empty payload test .
Basically without payload and with that 40 kpounds , it was like if Shuttle was already full . So added to that a payload , it was a way overweight Shuttle .
So bad results on abort with full payload might be linked to that . An extra 40000 pounds outside of the envelop
I will test that . But removing like we said those 40000 pounds will give us much more realistic results to compared with real data’s.
As for the flight path . It is te gamma value , angle between local horizontal and velocity vector at meco.