ramana wrote:Was the new larger diameter payload fairing flown with Russian cryo? That would answer the question. If it was then its a non issue and could be a mfg issue. If it was not flown earlier then the aero-loads need to be revisited. Earlier report said ISRO felt that the aero-loads were non issue as the larger diameter fairing was flown on the Indian cryo-stage and did not have early flight problem implying these aero-loads were not important. However that begs the question was the larger diameter fairing flown with the older Russian cryo-stage?
Another thing would be the thickness of the shroud in the connector area. How comparable are they between the Russian cryo-stage and the ISRO cryo-stage? If the thickness is lesser for Russian stage then it could be a pointer for it could deform.
The larger payload fairing was not flown with the Russian stage. But, I would be reasonably certain that ISRO had calibrated the stage to sustain higher loads (aerodynamic and extra weight). I could be wrong here and maybe ISRO hadn't taken the additional aerodynamic forces due to larger payload fairing into account but that would be too big a letup by such a competent organization.
I'll try to pictorially explain where the failure occurred. I had a chat with a friend to confirm what exactly the shroud mentioned here is. Although we can't be 100% sure, I believe I'm reasonably certain about this.
In the above picture, the black covering below the the stage (surrounding the engine nozzle and containing all the cables etc) is/contains the shroud. Several connectors are also visible. This particular picture was sent by a friend and is not the GSLV upper stage.
Now lets take a look at the GSLV upper stage. (This one is the indigenous one but russian one would be very similar)
In this picture pan right from the uncovered interstage (nozzle) and you can see the connectors fixed on metal plates (brown plate with silver connectors). So my guess here is that shroud in question here is the interstage shroud (interstage covering) shown in the first picture and still not covered in the GSLV picture above. This got deformed due to flight load.
Reference:
The German made connectors are fixed on a metal plate. The plate, in turn, is fixed to a shroud or cylindrical cover that comes between the cryogenic engine and the lower stage (engine).
According to Nair, the shroud made of composites is part of the Russian cryogenic engine and it got deformed due to the flight load.