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- Mar 28, 2008
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The problem is that after requesting the burn data the first time, the S-IVB changes it’s attitude according to that. Because the S-IVB has attitude thrusters only at its rear end, there’s a rather huge “translational component” during that manoeuver, that means the S-IVB changes it’s orbit slightly. After the manoeuver, the S-IVB requests the burn data again with the hope to get new burn data w.r.t. it’s now-current orbit. Then it changes its attitude again according to that, requesting again and so forth for a couple of times.
It's possible to press [EXE] after S-IVB orientation to re-compute the data but I didn't do that in my test. Also set the TIg mode to manual before that. Also note that [EXE] shouldn't be pressed when time to ignition is less than 300 seconds. I'll try to remove that limitation from manual TIg mode.
I will be retrying the scenario ASAP