Any word on whether they solved that problem?
Am I mistaken? The last two launches had a last second abort due to over-pressure in the engines. Any word on whether they solved that problem?
Unlike the previous flight, it appears there isn't an umbilical going directly to the Dragon, only the combo umbilical to the trunk and then to Dragon via the "Dragon Claw". How do they get conditioned air to the pressurized section? I had assumed the "Dragon Claw" was only for power, data and liquid coolant. Can they use active cooling while on the pad?
Quote from: corrodedNut on 03/01/2012 07:00 pmUnlike the previous flight, it appears there isn't an umbilical going directly to the Dragon, only the combo umbilical to the trunk and then to Dragon via the "Dragon Claw". How do they get conditioned air to the pressurized section? I had assumed the "Dragon Claw" was only for power, data and liquid coolant. Can they use active cooling while on the pad?Usually, capsules don't get conditioned air because it is pressurized.
NASA TV video of the terminated attempt earlier: