I took the speed data from SpaceX’s stream at intervals of 30 frames and plotted the acceleration.

In his analysis video, Scott Manley mentions a puff at T+7:06 which corresponds to an increased rate of LOX consumption. He may well be right, but I wonder if there is more going on here.

At T+7:39, there is a much more aggressive puff which corresponds to the acceleration flattening to a constant rate. Previously it was increasing (constant thrust and decreasing vehicle mass) though I can’t say if it was linear or exponential. It would be fascinating to know what was happening throughout the rest of the burn.

I did a quick web search to see if the Falcon 9 second stage does a similar thing during terminal guidance, but found no such indication. I admit I did not do the analysis myself.

So what do you think? Were the last 30 seconds part of the throttle profile or an indication of another more energetic event that doomed the flight?

I’m sure we’ll find out for sure from the investigation report, but I thought it would be fun to speculate a little! :)

  • @llamacoffeeOP
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    31 year ago

    Yeah I really messed up the units on this one. It’s actually in km/hr/s, which makes it around 35m/s^2. My bad!

    • @[email protected]
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      41 year ago

      Well my calculations are based on the units you meant to use. What I wrote is true based on km/h/s.