There were multiple unexpected "energetic events" seen by observers apparently due to some of the engines failing around liftoff. These "energetic events" could have contributed to greater than expected downward force under the launchpad. If correct, it seems positive that the excess energy was directed downward still permitting the liftoff. That the ship was able to continue the flight through Max-Q and up to MECO and starting the separation spin maneuver seems like a very positive sign. I believe they've already started construction of upgraded launch facilities which include fire trenches and water deluge systems. This first launch facility was basically a V 0.1 test and it appears to have done its job of getting a Starship test article in the air. It's important to remember their development strategy is pipelined and intentionally test-to-failure with multiple improving prototypes in simultaneous parallel construction. Today's test ship was already several versions old.
Also, the rocket didn't exactly "blow up", it apparently lost attitude control during the separation spin maneuver and couldn't achieve the parameters necessary for stage separation. The subsequent rotations appeared to be attempts at automated attitude recovery. The eventual termination was a controlled FTS initiated when SpaceX determined the flight was unrecoverable. I found it incredible that a supersonic rocket about twice as big as anything humans have ever launched was able to rotate several times at around 1300 Mph and over 100,000 ft altitude while maintaining structural integrity. Fortunately, it appears they were able to delay detonating the controlled demolition charges long enough to receive the vital telemetry data that was the entire reason for today's test. That this early prototype managed to load fuel, pressurize, ignite engines, clear the tower, reach MaxQ, MECO, start the separation turn and then down link all the data makes it a massive success from SpaceX's perspective. Everything after MaxQ was pure bonus territory. The engineers at SpaceX must be thrilled to be ingesting all that sweet data from hundreds of internal sensors and start comparing real-world performance against their simulation models.
"test-to-failure" means that when you realize you may have made a mistake, you don't automatically scrap all your work to fix the mistake before continuing down the development path. You complete that prototype and test it because there are a thousand more mistakes to discover. Even if the known mistake will for sure result in a catastrophic failure, there may still be a large window of opportunity for productive mistake discovery before that for-sure failure ends that test run. You want to discover and fix mistakes in parallel, not serially.
Obviously there are judgment calls for when a mistake might prove too costly even in a test run. But manifestly SpaceX has damn good judgment in that regard. If you don't like how the sausage is made, just avert your eyes; don't complain about how ugly the sausage making process is.
From the launch commentary, the rocket is designed to do a 180 at that altitude for the separation event. So a couple extra rotations isn’t going to hurt anything. Additionally, air density at 100k ft is ~1/80th of sea level, which helps.
You mean it should have separated on a 180-flip? Boosting rocket all the way there to break and start orbiting in opposite direction? No way. F9 doesn't do that. The booster should have flipped without starship. That was mistake on commentator side - they were talking all the time like everything is normal. Even when we all saw it started to twist, commentator sayd something like: waiting on separation.
Anyways, the stress rocket experiences in a position like that is such that they break up, because its not designed for positions like that - we have seen that on failing rockets videos. This one did multiple flips with upper stage attached that shouldn't be there on rotation. And thats great :)
Also, the rocket didn't exactly "blow up", it apparently lost attitude control during the separation spin maneuver and couldn't achieve the parameters necessary for stage separation. The subsequent rotations appeared to be attempts at automated attitude recovery. The eventual termination was a controlled FTS initiated when SpaceX determined the flight was unrecoverable. I found it incredible that a supersonic rocket about twice as big as anything humans have ever launched was able to rotate several times at around 1300 Mph and over 100,000 ft altitude while maintaining structural integrity. Fortunately, it appears they were able to delay detonating the controlled demolition charges long enough to receive the vital telemetry data that was the entire reason for today's test. That this early prototype managed to load fuel, pressurize, ignite engines, clear the tower, reach MaxQ, MECO, start the separation turn and then down link all the data makes it a massive success from SpaceX's perspective. Everything after MaxQ was pure bonus territory. The engineers at SpaceX must be thrilled to be ingesting all that sweet data from hundreds of internal sensors and start comparing real-world performance against their simulation models.