Author Topic: LIVE: SpaceX - Falcon I (Mk.II) NET March 20 (Attempt 2)  (Read 265153 times)

Offline Chris Bergin

I should say, before we write up some post launch article from Elon quotes, that I think what we've just seen is astonishing. Well done SpaceX.
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Offline Chris Bergin

Quote
nacnud - 21/3/2007  2:30 AM

The staging is at T+2:52 and the oscillations aren't redialy apparent until T+4:30. That's a fair time difference

And it's the last 15 seconds where the view of the Earth really starts to wander (roll problem).
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Offline Danderman

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RE: LIVE: SpaceX - Falcon I (Mk.II) NET March 20 (Attempt 2)
« Reply #402 on: 03/21/2007 01:45 am »

Quote
Chris Bergin - 20/3/2007  7:42 PM  I should say, before we write up some post launch article from Elon quotes, that I think what we've just seen is astonishing. Well done SpaceX.

Indeed, a great achievement. 


Offline Eeyore3061

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Re: LIVE: SpaceX - Falcon I (Mk.II) NET March 20 (Attempt 2)
« Reply #403 on: 03/21/2007 01:46 am »
Quote
Danderman - 20/3/2007  10:39 PM

Quote
JonSBerndt - 20/3/2007  7:36 PM  Question: What is the arrangement of the ullage motors on Falcon - assuming they have them to settle the fuel prior to second stage ignition? It seems as if there is something forcing a rate on the upper stage prior to ignition.Or, am I imagining things? Any estimates on qbar? Altitude and velocity at staging?  Jon

I was not aware that pressure fed engines require ullage motors.

 


Yes, to keep them from swallowing a bubble of pressurant.  

... and possably locking up the lines  ;)  

Michael.

Offline marsavian

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RE: LIVE: SpaceX - Falcon I (Mk.II) NET March 20 (Attempt 2)
« Reply #404 on: 03/21/2007 01:46 am »
a bold quote

'He doesn't foresee needing another test flight before launching the first operational mission in late summer carrying the U.S. military's TacSat 1 spacecraft.'

http://www.space.com/missionlaunches/sfn_070320_spacex_falc1cntdwn.html

Offline Danderman

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Re: LIVE: SpaceX - Falcon I (Mk.II) NET March 20 (Attempt 2)
« Reply #405 on: 03/21/2007 01:49 am »

Quote
Chris Bergin - 20/3/2007  7:43 PM   And it's the last 15 seconds where the view of the Earth really starts to wander (roll problem).

 

Although it did not seem like a very serious roll problem - in fact, if that were the only problem, it would be a non-problem, since a little roll is not a bad thing.  However, I noticed that after 4 minutes, when the oscillations began, the launch crew became very tight lipped.

On the other hand, the circular oscillations were worrisome. 

 

 


Offline yinzer

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Re: LIVE: SpaceX - Falcon I (Mk.II) NET March 20 (Attempt 2)
« Reply #406 on: 03/21/2007 01:50 am »
Severe pogo could cause the loss of telemetry easily - high amplitude vibrations will lead to structural failure, and could easily knock the batteries powering the stage loose.  I wonder if Elon was watching the video feed, as on slow-motion replay it clearly shows that the interstage it the second stage nozzle.

harryw: I suggest you write to SpaceX and tell them that if they don't continue to broadcast video after the launch failure, there's no way you're going to buy a rocket from them.  Surely when faced with the loss of business they will change their ways.
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Offline Chris Bergin

Quote
daveglo - 21/3/2007  2:40 AM

I'll throw my $0.02 in with the other folks offering congratulations to SpaceX.  Take the partial success, and build on it.  So it wasn't perfect.  So what?  It's still a bargain, even if it was sub-orbital.  300KM is nothing to sneeze at.
 
And thanks to Chris and the others for the L2 video, best turnaround time on the web!

Thanks to the webmasters, they are amazing. Fyi, we topped out at several thousand on at the same time. The forum counter is only a guide and was way off at one point due to the demand (something like 100 requests a second). They did very well in keeping us up (if a bit slow at times).
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Offline Danderman

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Re: LIVE: SpaceX - Falcon I (Mk.II) NET March 20 (Attempt 2)
« Reply #408 on: 03/21/2007 01:53 am »

Quote
yinzer - 20/3/2007  7:50 PM  Severe pogo could cause the loss of telemetry easily - high amplitude vibrations will lead to structural failure, and could easily knock the batteries powering the stage loose.

 Well, that is certainly true, but when I wrote "severe pogo" I was not thinking of "tear the vehicle apart" pogo.

 But let me ask the crew here: what failure modes WOULD cause the telemetry to cease? Discounting, of course, coincidental telemetry or electrical problems.

 


Offline WHAP

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Re: LIVE: SpaceX - Falcon I (Mk.II) NET March 20 (Attempt 2)
« Reply #409 on: 03/21/2007 01:54 am »
Quote
Eeyore3061 - 20/3/2007  8:46 PM

Quote
Danderman - 20/3/2007  10:39 PM

I was not aware that pressure fed engines require ullage motors.

 


Yes, to keep them from swallowing a bubble of pressurant.  

... and possably locking up the lines  ;)  

Michael.

I haven't heard them called "ullage motors" before, but I doubt they would do any good before the second stage's first burn.  They are usually very low thrust and would not have had much of an effect in the short time from separation to engine burn.
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Offline Mark Max Q

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Re: LIVE: SpaceX - Falcon I (Mk.II) NET March 20 (Attempt 2)
« Reply #410 on: 03/21/2007 01:56 am »
Wonderful launch. Rewatching on L2, really was a great cam shot on the way up. Well done SpaceX

Offline kevin-rf

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Re: LIVE: SpaceX - Falcon I (Mk.II) NET March 20 (Attempt 2)
« Reply #411 on: 03/21/2007 01:59 am »
Just some thoughts before signing off for the night...

The first flight fire was due to a busted nut that count not tolerate the salt water enviroment.
Mondays abort was due to a timeout set shorter than reality.
Tonights first abort was triggered by an engine pressure being 0.1(?) psi out of spec.
It looks like the tolerances where to tight on staging causing recontact?
Then we had the oscillations set in. An overdamped (over correcting) control loop?

I don't know, looks like they designd it to the simulations not taking into account real world slop and tolerances. Which goes back to the discussions we where having earlier tonight about needing more real world testing and less reliance on simulation.

That said it, it was a test flight, providing real world experience, they recovered from an on pad abort with engine ignition, they had an excellent first stage flight and by the sounds of it with some good wind shear, It sounds like they learned a fair amount (which divereges from the simulations) about the second stage flight regime.

Hats off, better luck next time.
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Offline nathan.moeller

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Re: LIVE: SpaceX - Falcon I (Mk.II) NET March 20 (Attempt 2)
« Reply #412 on: 03/21/2007 01:59 am »
Beautifully done SpaceX!  Congratulations to you all on making it to space on the second try.  Truly a remarkable feat.  Looking forward to the next flight!
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RE: LIVE: SpaceX - Falcon I (Mk.II) NET March 20 (Attempt 2)
« Reply #413 on: 03/21/2007 02:02 am »
Quote
marsavian - 20/3/2007  8:46 PM
a bold quote
'He doesn't foresee needing another test flight before launching the first operational mission in late summer carrying the U.S. military's TacSat 1 spacecraft.'

http://www.space.com/missionlaunches/sfn_070320_spacex_falc1cntdwn.html

Well at least he's consistently in character.  You have to be a bit arrogant to lead a bunch of scientists, engineers, techs, and associated riffraff :-).  He's also demonstrated that he can and does learn.  Oh, to be a fly on the wall tomorrow back in El Segundo...
 

Next up is more learning curve:  Bring on the various government inspectors associated with launching a US asset.

DCMA, anyone?

 


Offline WHAP

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Re: LIVE: SpaceX - Falcon I (Mk.II) NET March 20 (Attempt 2)
« Reply #414 on: 03/21/2007 02:03 am »
Quote
Danderman - 20/3/2007  8:53 PM

But let me ask the crew here: what failure modes WOULD cause the telemetry to cease? Discounting, of course, coincidental telemetry or electrical problems.

I guess an explosion would cause "coincidental telemetry or electrical problems".  I've seen video from Delta II boosters continue while they tumbled back to earth after separation.  The signal starts to break up and become intermittent, not abruptly end as it did tonight.  However, I'm not going to criticize SpaceX for that - it's their video, and it's their prerogative to turn it off when they want.

What started the discussion about pogo?  Would you expect to see that type of engine movement in response to pogo?
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Offline JonSBerndt

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Re: LIVE: SpaceX - Falcon I (Mk.II) NET March 20 (Attempt 2)
« Reply #415 on: 03/21/2007 02:03 am »
Quote
Eeyore3061 - 20/3/2007  9:46 PM

Quote
Danderman - 20/3/2007  10:39 PM

Quote
JonSBerndt - 20/3/2007  7:36 PM  Question: What is the arrangement of the ullage motors on Falcon - assuming they have them to settle the fuel prior to second stage ignition? It seems as if there is something forcing a rate on the upper stage prior to ignition.Or, am I imagining things? Any estimates on qbar? Altitude and velocity at staging?  Jon

I was not aware that pressure fed engines require ullage motors.


Yes, to keep them from swallowing a bubble of pressurant.  

... and possably locking up the lines  ;)  

Michael.

From the SpaceX web site:

"Helium pressurization is again provided by composite over wrapped inconel tanks from Arde. However, in this case the helium is also used in cold gas thrusters for attitude control and propellant settling when a restart is needed."

Prior to second stage ignition, I would guess that there is a slight negative acceleration. As Michael points out, pressure alone isn't going to keep a liquid propellant at the right end of the tank. :)

It occurred to me that this might possibly be a failure mode [referring to what caused the engine bell ding]: a stuck or failed second stage cold-gas thruster. Maybe ...

Regardless, I'll add my congratulations to SpaceX. A very exciting day.

Jon

Offline yinzer

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Re: LIVE: SpaceX - Falcon I (Mk.II) NET March 20 (Attempt 2)
« Reply #416 on: 03/21/2007 02:06 am »
Loss of attitude control could have blocked antenna line of sight.  Or they could have cut the signal when things went south.

Looked like they had a staging problem, which is not surprising as staging is hard to test under representative (zero-G, vacuum) conditions.  It still worked a lot better than I thought it was going to, although I have to say once second stage flight started, I wondered if it might make it all the way.  Congratulations to them for getting as far as they did, better luck next time.

As for being full of hubris, well... Elon cut his teeth in the dot-com world - talking a big game is par for the course there.  Falcon 9 and Dragon seem overly grandiose, but if my understanding of things is correct, the phase 1 COTS contracts are all pay-for-performance, and phase 2 could end up going to ATV-on-Atlas-V.
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Offline aero313

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RE: LIVE: SpaceX - Falcon I (Mk.II) NET March 20 (Attempt 2)
« Reply #417 on: 03/21/2007 02:09 am »
Quote
Stargazin2nite - 20/3/2007  10:12 PM

Danderman -- good point -- I just checked the payload in more detail and it does look like instrumentation to characterize the launch.  At first I was under the impression that DARPA was adding an additional functional satellite, but that appears not to be the case.

In any event, I am still amazed that a company with only 250 people have accomplished this!  :)

Orbital had abour 150 people when Pegasus had a successful maiden flight.  As with SpaceX, some of those were working other programs at the time.

Offline Chris Bergin

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Online Nate_Trost

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Re: LIVE: SpaceX - Falcon I (Mk.II) NET March 20 (Attempt 2)
« Reply #419 on: 03/21/2007 02:13 am »
Someone has also posted a version up on YouTube:

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