Are we a "Go" for 3:44 AM EDT?
Quote from: Garrett on 05/21/2012 09:44 amQuestion: does the N2 for purging the pumps come from onboard tanks or from an umbilical link to the pad?I case you're wondering, IIRC the red bottles attached to the bottom of the second stage perform this function for Merlin Vac.
Question: does the N2 for purging the pumps come from onboard tanks or from an umbilical link to the pad?
Wouldn't it have helium spheres inside the tank for that?
Quote from: ugordan on 05/21/2012 02:32 pmWouldn't it have helium spheres inside the tank for that?Yeah, the users' guide says heated helium for tank pressurization.
GO for the 22nd. New thread for that. Will keep this one going for a while.
That's good; increases the likelihood that it was a software-based problem (over-conservative red lines in the engine health monitoring software) rather than something genuinely wrong with engine #5's injectors or combustion chamber.
Quote from: Ben the Space Brit on 05/21/2012 06:05 pmThat's good; increases the likelihood that it was a software-based problem (over-conservative red lines in the engine health monitoring software) rather than something genuinely wrong with engine #5's injectors or combustion chamber.You haven't been paying attention lately, have you?
A check valve that allows the nitrogen purge prior to ignition in the Merlin engine was stuck open just before launch. This stuck valve allowed “liquid oxygen to flow from the main injector [for the rocket engine itself] into the gas generator injector” that generates hot turbine gas, which drives the turbopumps, according to SpaceX. The turbopumps are basically very high-powered fuel and oxidizer pumps that deliver the liquids to the main combustion chamber of the rocket. The result was the turbopumps were operating at a slightly higher power level, resulting in the high pressure detected in the combustion chamber on engine five.
Is't it times for a LAUNCH ATTEMPT 2 Updates thread?