Can someone remind me (I'm sure it's been explained before) why the ET insulation is on the outside of the tank, rather than inside the skin?
IIRC, the Saturn 5's S-II stage had the insulation under the skin. Why not with the ET?
Cheers
Can someone remind me (I'm sure it's been explained before) why the ET insulation is on the outside of the tank, rather than inside the skin?
IIRC, the Saturn 5's S-II stage had the insulation under the skin. Why not with the ET?
Cheers
Don't want to contaminate the liquid with anything lining the tank. Not to foul pumps etc. Also, ice build-up on the outside.
Of course, they "Could" seal the foam with epoxy FRP. Weight and expense.
Nothing's easy.
Dan
FRP is HEAVY. That would vastly increase the weight.
I would also assume that the tank and the skin work off each other for strength. Any separation between the two would require much more of a structure.
First the design requirements were overall very different. Second, ice forming on a traditional rocket is not an issue (provided it falls off).
Do you remember all those sheets of ice falling off a SatV launch? I would assume there was considerably less insulation. (Fill and go...)
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