Okay. So, does this failure have anything to do with the previous Soyuz failure? I understand that the 2.1-b has a different third stage then on the previous Soyuz.
Some basic data:Progress is launched by Soyuz-U.Soyuz TMA-M is launched by Soyuz-FGMeridien is launched by Soyuz 2-1bThe difference between Soyuz-U and Soyuz FG are the combustion chamber injectors, and allegedly, some quality control procedures.The difference between Soyuz-FG and Soyuz 2-1b are the avionics (Soyuz 2-1b has a digital flight control system, whereas Soyuz FG is analog) and the 3rd stage of Soyuz 2-1b is significantly different - it uses a different engine and the prop tanks are different, although the stage is externally identical.If the 3rd stage engine stopped burning some seconds into flight, it would be seem to be the same type of failure as the Soyuz failure earlier this year, although the engines are different.
The claim of a Tobolsk impact zone seems surprising given how late in the burn things failed... I would have expected it to be semi-near-orbital by +421s and make it to the Pacific, but I haven't run the numbers yet... does anyone have a feel for this?
Do we yet know what failed? Upper Stage or Staging etc?
Wow! NK magazine just asked a final question, in English
Quote from: JimO on 12/23/2011 03:30 pmWow! NK magazine just asked a final question, in EnglishWhat did he ask?
Wow! NK magazine just asked a final question, in English -- Popovkin scowled, stood up, and walked out without any further comments.