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They're talking about the center engine of the first stage, not the single engine of the second stage.


Yes. How would making that a different engine "introduce a single point of failure for the return part of the mission" that wasn't there already?


Because the return part of the mission relies on nine identical engines right now. So if one fails it is not a problem. But if you replace the central one with a different one that becomes critical for the return mission then you have made matters worse.


> Because the return part of the mission relies on nine identical engines right now. So if one fails it is not a problem.

Is that true? Doesn't the landing have to use the center engine - any other single engine would be asymmetric, and multiple engines would have too high a thrust.


Yes, if the center engine fails, the landing fails. There's no way to recover from that.

But the great thing about SpaceX's system is that it starts with a cheap expendable rocket, then makes it recoverable. You lose one? Who cares, build another one. They could have a 50% success rate recovering the first stages and it would still make things amazingly cheaper.


For future reference, the return part is made up of 3 burns. The first two use three engines, and the landing burn uses just the one. Coming back, it's obviously much lighter without all the propellant and 2nd stage/payload weight, so it needs much less thrust to reverse course. See http://flightclub.io for more info.




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