Hi all.
I am new to the forums but I have some experience with Orbiter already. I'm trying to do a precise reentry with Soyuz TMA (the one with ISS v3.2). I'm confused about what should I do after the de orbit burn. I have several questions:
- The most important is attitude. I do the burn retrograde, of course. Should I maintain retrograde after the burn? When should I disable the autopilot?
- When should I jettison the modules? This doesn't seem to have a great effect but I'd like to know how it's done.
- I have use the recomended procedure of the manual (ApA 380km to PeA 60 km at 167º) and also tried with BaseSyncMFD, which gives different parameters. I'd like to stick to the realistic parameters, which are right?
- I use controlled reentry and G goes to 8 or 9 every time. The manual says it should go to 4. What am I doing wrong? How should I maneuver the capsule, should I try to keep pitch to 0 or something else?
Thank you very much. I have been trying to find info on this issues but I haven't. I hope this is not a duplicate.
I am new to the forums but I have some experience with Orbiter already. I'm trying to do a precise reentry with Soyuz TMA (the one with ISS v3.2). I'm confused about what should I do after the de orbit burn. I have several questions:
- The most important is attitude. I do the burn retrograde, of course. Should I maintain retrograde after the burn? When should I disable the autopilot?
- When should I jettison the modules? This doesn't seem to have a great effect but I'd like to know how it's done.
- I have use the recomended procedure of the manual (ApA 380km to PeA 60 km at 167º) and also tried with BaseSyncMFD, which gives different parameters. I'd like to stick to the realistic parameters, which are right?
- I use controlled reentry and G goes to 8 or 9 every time. The manual says it should go to 4. What am I doing wrong? How should I maneuver the capsule, should I try to keep pitch to 0 or something else?
Thank you very much. I have been trying to find info on this issues but I haven't. I hope this is not a duplicate.