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pat bahn's avatar

Good article will but you probably should have dug in more on key details 1) this was a suborbital flight. So they achieved about 85% of orbital velocity and didn’t demonstrate a deorbit burn. So they either needed to load more propellant or they have to shave weight off the vehicle. 1A) given the relatively weak unstick I don’t think they can add more propellant 2) the lower velocity also means higher reentry velocity and lower peak temperatures and loads. The tps was failing on reentry in the Indian Ocean. They could easily have had more problems with burn through and control. It looks like they need a better tps adhesion solution and a stronger heavier TPS. That’s going to make the weight loss issue worse.

Now maybe they can send the design through the system. Next flight is supposed to be V3. That design is likely already frozen but maybe they can get to v4 with say 11

More engines on the base booster and maybe stretch the upper stage..

That may have enough margin for orbit. Not sure if they will be able to use the existing towers and building or if they have to build bigger.

They have clearly bounded the problem more.

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DrBDH's avatar

If you take enough ketamine, though, it was a rousing success! Only a small explosion! Only one engine failed! This is “only one window blew out of my airliner” level of success. Or, the level of engineering expertise America is doomed to experience for years to come.

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