Falcon 9 GEO Transfer Mission
spacex.com
spacex.com
listened back to the stream
"abort abort abort - props con(?) abort"
at about 1h:58m in the stream
EDIT : announcer did say that engineering stopped it because they hadn't done their review. Maybe the "abort abort abort" wasn't as dramatic as it sounded
"We called manual abort. Better to be paranoid and wrong. Bringing rocket down to borescope engines ... Elon Musk (@elonmusk) "
"Increasing helium spin start pressure. Probably <50%
chance of passing all aborts, but worth a try. Countdown
resuming "
https://twitter.com/elonmusk/status/406205240040771584
So it was unlikely they would go when they restarted the countdown.Update: Problem was the slow ramp up of the thrust of the rockets. Engineers are looking at the data. Rocket is on stand-by to launch today, but the commentator sounded skeptical.
Update: Clock was restarted with T-00:25:10, still some problems to resolve.
Update: Aborted on time T-48 seconds. Done for today. The rocket will be inspected and another launch attempt will be in a few days.
T minus 10min. Go SpaceX!
EDIT: It's impressive they were able to abort safely after ignition. That's historically rare, isn't it?
The wiki page is a pretty interesting read: http://en.wikipedia.org/wiki/Mercury-Redstone_1#Test_backgro...
I'm not sure how rare it is with liquid fueled rockets, but I know it's not even possible on solid fueled rockets (like the Shuttle's two boosters).
http://www.airspacemag.com/space-exploration/abort.html
I don't recall that happening with the Saturn V or other early rockets, apart from the accident Crito mentioned.
Liquid-fueled engines are inherently restartable. Otherwise, you wouldn't be able to test an engine without throwing it away afterwards.
Sometimes manual intervention is required, though. For example, the starter cartridge on the Titan was a consumable part, and had to be replaced before restarting the engine.
http://www.youtube.com/watch?v=vPW7ZqtW5U4
The footage is indeed amazing though.
> The Saturn V rocket was 111 meters (363 feet) tall, about the height of a 36-story-tall building, and 18 meters (60 feet) taller than the Statue of Liberty. Fully fueled for liftoff, the Saturn V weighed 2.8 million kilograms (6.2 million pounds), the weight of about 400 elephants. The rocket generated 34.5 million newtons (7.6 million pounds) of thrust at launch, creating more power than 85 Hoover Dams. A car that gets 48 kilometers (30 miles) to the gallon could drive around the world around 800 times with the amount of fuel the Saturn V used for a lunar landing mission. It could launch about 118,000 kilograms (130 tons) into Earth orbit. That's about as much weight as 10 school buses. The Saturn V could launch about 43,500 kilograms (50 tons) to the moon. That's about the same as four school buses.
To get some rough idea of scale, this blueprint shows a person near the engine / nozzle / thing.
Also said that if not today, they have more or less the same window tomorrow
EDIT: someone just said starting the clock momentarily ... looks like they might be going again
It seems that the checks failed here and the flight computer aborted launch at T+00:01.
if enginesOperational {
// TODO(rocketman): Remove this before the actual launch
panic("bail out for testing")
}Compared to later programs, there's also a "wow" in that NASA was "going to put some men on the moon", vs. the "space truck" paradigm of the Shuttle and other launches which at best send probes to far off planets and such. A different scale in every way.
Edit: Flight computer has aborted after engine fireup.
Edit: Failed was the wrong word, aborted is the correct term.