Star Voyager
Space Shuttle Refugee
- Joined
- Oct 25, 2008
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Engine test rescheduled for tomorrow.
SpaceX as they own the vehicle and pad. And this is a SpaceX demo launch of the Falcon 9, the Dragon on top is a complete dummy. NASA only pays for the cargo in the Dragon if it gets to ISS intact. If it doesn't, SpaceX won't see a cent of NASA COTS/CRS money.As long as the launchpad isn't seriously damaged by the launch, it's ok !
Which makes me think... Who would have to pay the repairs ? NASA or SpaceX ? :hmm:

SpaceX has provided the following statement after today's static fire attempt: "Today SpaceX performed our first Static Fire for the Falcon 9 launch vehicle. We counted down to T-2 seconds and aborted on Spin Start. Given that this was our first abort event on this pad, we decided to scrub for the day to get a good look at the rocket before trying again. Everything looks great at first glance."
"We completed pad preps on time and with good execution. The integrated countdown with the range included holdfire checks, S-band telemetry, C-band, and FTS simulated checks. We completed helium, liquid oxygen (LOX), and fuel loads to within tenths of a percent of T-zero conditions. Tanks pressed nominally and we passed all Terminal count, flight software, and ground software abort checks right down to T-2 seconds. We encountered a problem with the spin start system and aborted nominally."
"As part of the abort, we close the pre-valves to isolate the engines from the propellant tank and purge the residual propellants. The brief flames seen on the video are burn off of LOX and kerosene on the pad. The engines did not ignite and there was no engine fire."
"We detanked and safed the vehicle and launch pad. Preliminary review shows all other systems required to reach full ignition were within specification. All other pad systems worked nominally. Inspections will be complete tonight. Tomorrow will consist of data review and procedure updates. Commodities will be replenished tomorrow including TEA-TEB load, LOX and helium deliveries."
"We'll look to do the next static fire attempt in three or four days."
I assume the "spin start" referred to is the spinning up of the turbo pump shaft. Any one know what equipment is used to accomplish this? Obviously the pre-burner can't function until the turbo pumps have at least some momentum...
So TEA/TEB are used to start the turbine as well as to ignite the engine?In this case, the acronyms TEA and TEB are the key word what was used:
Didn't the Falcon 1 abort an engine start once and then go on to launch within a few hours anyway? I know they can recycle these Falcons at an amazing speed after a scrub. If nothing else comes from the program, their pad system alone is quite remarkable.