I didn't realize fuel could get too cold; how so?
I don't know specifics about the Falcon 1, but with liquid propulsion, you often have to preheat the cryogenic fuel before it goes into the combustion chamber. This is usually achieved by circulating it around the nozzle (which provides the dual effect of cooling the nozzle). If you allow the fuel to get too cold, the exhaust gas isn't as hot as it could be and you see a drop in the thrust.
In fact, unless I'm mistaken, you want the exhaust gases as hot as possible. The limiting factor is usually the thermal limits of the nozzle material.
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Webcast hasn't 'resumed' yet.
And interestingly the hold is now for 55 minutes, not 16. I guess they're taking a big step back.
How big is their launch window? (Or do they not have a target?)