SpaceX's Fourth Launch Attempt RSN
jcgam69 writes "SpaceX's Falcon 1 is on the pad in the South Pacific Kwajalein Atoll ready for its fourth launch attempt, according to a blog post over the weekend from SpaceX CEO Elon Musk. The countdown is scheduled for Tuesday, Sept. 23, between 4 p.m. and 9 p.m. PDT, though the launch window will extend through Thursday if need be."
From an email I received this morning from the SpaceX news mailing list:
The static fire took place on Saturday [20 Sep 2008, CA time], as expected, and no major issues came up. However, after a detailed analysis of data, we decided to replace a component in the 2nd stage engine LOX supply line. There is a good chance we would be ok flying as is, but we are being extremely cautious.
This adds a few extra days to the schedule, so the updated launch window estimate is now Sept 28th through Oct 1st [CA time].
It should be illegal to say that freedom of speech should be limited.
Listen, lad. I built this kingdom up from nothing. When I started here, all there was was swamp. Other kings said I was daft to build a castle on a swamp, but I built it all the same, just to show 'em. It sank into the swamp. So, I built a second one. That sank into the swamp. So, I built a third one. That burned down, fell over, then sank into the swamp, but the fourth one... stayed up! And that's what you're gonna get, lad: the strongest castle in these islands.
None of them can see the clouds; The polished wings don't care.
I'm all for learning from my mistakes, but how much do these things cost to build and launch? You have to admire the dedication though - sinking that kind of money from your own pocket into something like this takes some guts. If he pulls it off, he might have something.
-=- I tried going insane, and it was fun for a while, but I got bored and decided to go sane. -=-
http://www.spacex.com/updates.php
They should use a trebuchet. Can't be any worse than what they've tried already,
Confucius say, "Find worm in apple - bad. Find half a worm - worse."
So do all those very combustible looking trees fold over at launch like those ones in Thunderbirds?
Seriously, while I appreciate their tenacity, these attempts weren't news the last time either. Please skip the "here they go again" post and just let us know how it went, ok?
Wake up - the future is arriving faster than you think.
Good luck to them! Space-X has already won the stick-to-it award for persistence-- now let's hope they win the "great-success-after-hard-work" award.
http://www.geoffreylandis.com
"What goes up, better doggone stay up!"
-Ours is the wisdom of Solomon, the magic of Merlyn, the fall of Icaris.
They did pay for the first 2. The last one and this one are on Spacex's dime. As to the # of failures, EVERY group that has started with rockets has a number of failures up front. Once they have their first couple of successes, then it tends to be with new versions (though the shuttle says otherwise).
I prefer the "u" in honour as it seems to be missing these days.
Just a suggestion.
"As it turned out, a very small increase in the time between commanding main engine shutdown and stage separation would have been enough to save the mission."
If the residual thrust was the problem I would think that an accelerometer would act as a good safeguard. Heck I would thing that the INS could provide this input.
See my blog http://ilovecookes.blogspot.com/ for light hearted technical information.
Not relevant to TFA, but to the /. crowd:
Unix/Linux admin and software engineer positions open at the L.A. facility. https://spacex.com/careers.php
The subject line is a ripoff of a ST:TNG episode. I'm not with SpaceX. I'm still trying.
"I may be synthetic, but I'm not stupid." -- Bishop 341-B
so like, do you think crowbars are effective in space? where do i send it?
They could use a few cues from Cid circa FFVII and avoid potential catastrophe by rechecking the oxygen tanks BEFORE initiating the launch sequence, lest they have another rocket sitting in the middle of nowhere due to a lack of funding.
What does that mean? It's not defined in the summary or the article and google returns crap for "define:rsn" and "spacex rsn".
If it's "Real Soon Now" as acronymfinder suggests, then the summary writer and editor both suck.
Minor point, but at approximately 8 deg 43 min N, 167 deg 44 min E would Kwajalein not be in the Northern Pacific or at least Central Pacific?
So they're the ones who've been creating all those forum spam accounts!
Is the use of an accelerometer to control second stage separation the norm? (I am neither a rocket scientist nor a rocket engineer, but I would like to know.)
Also, are ullage motors normally used for stage separation engine starts, or are they reserved for engines starts after a longer weightless perion?
I've got grave doubts about any company whose CEO has a name that sounds more like a perfume brand.
Would really like to see this attempt succeed. Many of the Google Lunar X PRIZE teams are relying on it, and this would be an excellent first step in that direction.
http://www.googlelunarxprize.org/lunar/about-the-prize/preferred-partners
I would think accelerometers aren't used. Another point of failure and all.
-Bucky
Ullage is used for stage separation too. The Saturn V had big'uns. The motors didn't separate the stages, they provided a little acceleration to settle the fuel at the back (bottom) of the tank before the stage ignition.
You see them on each stage here.
http://upload.wikimedia.org/wikipedia/commons/b/b2/Saturn_v_schematic.jpg
Fascism trolls keeping me up every night. When I starts a preachin', he HITS ME WITH HIS REICH!
Ullage is used for stage separation too. The Saturn V had big'uns. The motors didn't separate the stages, they provided a little acceleration to settle the fuel at the back (bottom) of the tank before the stage ignition.
You see them on each stage here.
http://upload.wikimedia.org/wikipedia/commons/b/b2/Saturn_v_schematic.jpg
So is the lack of an ullage motor on the Falcon 1 second stage likely to cause problems?
The second stage fires relatively soon after the first stage is done burning, so there's little time for propellants to move forward in the tanks. The Saturn had a relatively longer gap between first and second stage burnouts so ullage motors were included. The later Saturns actually removed the ullage motors from the second stage, since that one lit off just under 5 seconds after the first stage burned out.
Fascism trolls keeping me up every night. When I starts a preachin', he HITS ME WITH HIS REICH!
Atlas, the Titan who held the weight of the world on his shoulders.
"Victory means exit strategy, and it's important for the President to explain to us what the exit strategy is." G.W.Bush
What is this, an Issac Asimov novel?
What?
Yes, let's make all that advanced rocket design public information so anyone can build intercontinental ballistic missiles!
BRILLIANT!
Hey, Bin Laden come on out we've got free rocket designs! Still got any of those oil millions left to build one?
Hey Pyongyang, want to make better rockets? Here you go!
Well the INS has an accelerometer and if it fails then you are in a world of hurt. I would assume that they are redundant.
What I would suggest would be something like this.
waitX secs
check accelerometer.
If still getting thrust wait a bit more.
If wait time is getting too long stage anyway and hope for the best.
There has to be an optimum time to stage and a last chance time to stage.
But it is just an idea.
See my blog http://ilovecookes.blogspot.com/ for light hearted technical information.