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Could you give some info on why a water landing was chosen over land?
Does it save a significant amount of weight or is it just generally considered safer? Did recovery costs have any impact on that decision?
only_to_downvote14 karma
We already had to have a water landing capability to provide an abort capability.
I'm kinda ashamed to admit that I never considered that, but it makes a lot of sense. Thanks for the answer.
only_to_downvote251 karma
5 in total elongation
106 ft total length
5.2e-6 in/in/degF approximate coefficient of thermal expansion for Ti-6Al-4V (assumed Titanium alloy used, varies from ~4.8 to ~5.5 across temperature range of interest)
average skin temperature ~= 5in / (105ft * 12in/ft * 5.2e-6 in/in/degF)
~= 755 degF
Ever toast some marshmallows by holding them up against the side of the cockpit?
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