3DDave
Aerospace
- May 23, 2013
- 10,767
Per Wikipedia
So all joints would have the same burn exposure. It appears that most erosion events happened at the same field joint, the one near the nozzle.
Relevant discussion:
The propellant had an 11-pointed star-shaped perforation in the forward motor segment and a double-truncated-cone perforation in each of the aft segments and aft closure. This configuration provided high thrust at ignition and then reduced the thrust by approximately a third 50 seconds after lift-off to avoid overstressing the vehicle during maximum dynamic pressure (max. Q).
So all joints would have the same burn exposure. It appears that most erosion events happened at the same field joint, the one near the nozzle.
Relevant discussion: