My undestanding was that the ET foam was there to protect the shuttle from condensation icing that forms on the tank.<br /><br />In another thread, I mentioned not having foam on the Saturn V as an example of this because Shuttle_guy alluded to boiloff as the reason for the foam. I checked and found the Saturn V did indeed have foam sprayed on the tank. I was unable to verify if the tank is internal or the skin of the S-II serves as the actual tank wall. The best drawing of the S-II I could find did seem to indicate the LH2 tank is the skin of the S-II, plus Shuttle_guy said he actually sprayed foam on the S-II as a NASA or contractor employee. In any case, it was sprayed on much thinner than what is sprayed on the ET. The ET foam being up to 8 inches thick in some places and the Saturn V S-II was 1 inch if I recall the tech data correctly.<br /><br />In that case, the foam serves an additional purpose on the shuttle ET. I'm not up on the Falcon specs but if the upper stage is not cryogenic, theres no need for foam to prevent boiloff. <div class="Discussion_UserSignature"> <p><strong>My borrowed quote for the time being:</strong></p><p><em>There are three kinds of people in life. Those who make it happen, those who watch it happen...and those who do not know what happened.</em></p> </div>