The countdown process needs optimization. There are things missing and things which shouldn’t be there. We’re talking about speed of loading propellant, density of it, etc.
Then there’s software. So much software.
And a million other things. Rockets are complex, launching them doubly so.
Possible, but not a sure bet by any means and one I'd happily take the other side of.
At some point, your in silico model needs real world data to validate it.
A few
- How long fuel takes to load
- How much is lost due to venting, how fast we need to recycle that to keep the ship on the pad ready to launch
- Actual engine startup times when many starting at once
- Actual thrust as the vechicle leaves the pad
- Actual response to control authority (how fast the ship changes course) for vectoring, gas thrusters, flaps
- Actual vibration measurements, how much measured acceleration is noise
If that's true, then they can just fix whatever is wrong with the stage separation. And if it's something else, they can probably fix that too. Doesn't seem like it was anything unchangeably / structurally wrong with the entire craft.