Ground system issue scrubs first launch of SpaceX’s Starship V3 rocket

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I’m not really sure why this is spun as a positive thing for SpaceX. If something goes wrong on this flight and it’s a hardware issue then they have to go back and retrofit it on the already built hardware. As opposed to having the fix designed and built right the first time.

Depends entirely on what the issue is. They've already done static fire tests so they know the engine design works.
 
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I’m not really sure why this is spun as a positive thing for SpaceX. If something goes wrong on this flight and it’s a hardware issue then they have to go back and retrofit it on the already built hardware. As opposed to having the fix designed and built right the first time.
On the first launch of such a major redesign for a system this large and complex, everything going flawlessly would be a more than minor miracle - no matter how much care was taken in design up-front.

That said, SpaceX did spend a great deal of effort and time, over the past 6+ months, torture-testing some representative v3 test tanks and hulls using purpose-built, elaborate test rigs; and they have been pretty methodical and thorough with ground tests of the pad as well as the flight hardware. And the engines have been in intensive testing for about two years already; the current production version serial numbers for Raptor 3 are already in the 170's (and there were many pre-productuon builds and test articles before that). Still, despite all that, it's likely at least something will go wrong with flight 12.

SpaceX's ability to quickly analyze the problems, then retrofit and fly the next build, is a positive thing as it seems likely to result in v3 starting to fly actual payloads to orbit within a year.
 
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It sounds like all of the holds in those final seconds were due to problems with the launch structure and ground systems, not the rocket. It was the same thing with the scrub of Artemis II. I don't understand why ground systems seem to be the source of more scrubs than the rockets, which I would assume are much more complex?
 
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Barleyman

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It sounds like all of the holds in those final seconds were due to problems with the launch structure and ground systems, not the rocket. It was the same thing with the scrub of Artemis II. I don't understand why ground systems seem to be the source of more scrubs than the rockets, which I would assume are much more complex?
It's not called stage zero for nothing.
 
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shawnce

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It sounds like all of the holds in those final seconds were due to problems with the launch structure and ground systems, not the rocket. It was the same thing with the scrub of Artemis II. I don't understand why ground systems seem to be the source of more scrubs than the rockets, which I would assume are much more complex?
A lot of complex stuff happens in the ground system.

It is dealing with a massive amount of propellants that have to be delivered rapidly and safely to the craft… propellants that are cryogenic and generally hard to handle and maintain at the needed temperatures / densities.

Additionally a range of inert gases have to be used to chill and purge all of the complex plumbing on the ground and on the craft. It needs to keep the propellants pure as possible in the process (prevent unwanted gases mixing in, etc).

It also has to support the craft during all of this, detach from the craft at the correct times using complex mating ports that have to deal with electrical, hydrologic fluids, cryogenic inert gases, and cryogenic propellants, etc.

You also have the deluge system that requires a massive amount of water driven at very high pressures, etc. (actually gas generators built from a set of Raptor derived power heads, rocket engine pressuring the deluge system).

Then in the case of SpaceX the ground systems also have to deal with recovering the craft stages.

Anyway the ground system is often the most complex aspect of a launch system or at least one par with the craft itself.

In the case Artemis they are dealing with low cadence of launches with long gaps in ground system use which impacts repeatable reliability. Also hydrogen fuel sucks to deal with.

In the case of this launch they are dealing with a brand new ground system and tower. It will have teething pains for the first few flights.

…a lot of values, a lot of actuators, a lot of plumbing, a lot of monitoring systems, storage tanks, etc
 
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What's the track for the satellite mass simulators and close-range-photography-capable Starlinks? I would presume the lumps would follow their launch vehicle into approximately the Indian ocean, but are the operational ones going to burn like a bat out of hell to give themselves a longer mission or just dump data into the network until the plasma takes over?
 
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What's the track for the satellite mass simulators and close-range-photography-capable Starlinks? I would presume the lumps would follow their launch vehicle into approximately the Indian ocean, but are the operational ones going to burn like a bat out of hell to give themselves a longer mission or just dump data into the network until the plasma takes over?
The two modified Starlink v2 Minis will burn up with all the rest. They're not capable of significantly raising their orbits, quickly enough to survive the low-apogee, suborbital trajectory they're initially deployed into. And that's before taking into account the extra bolted-on mass to shoehorn them inside a Pez dispenser designed for much wider v3 satellites.
 
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The two modified Starlink v2 Minis will burn up with all the rest. They're not capable of significantly raising their orbits, quickly enough to survive the low-apogee, suborbital trajectory they're initially deployed into. And that's before taking into account the extra bolted-on mass to shoehorn them inside a Pez dispenser designed for much wider v3 satellites.
Ah, extra brackets would do that even more! I'm guessing that they can run fully internal until toast and won't need to deploy solar arrays, either. Should be another unique view from this development process (we've had a lot of those!).
 
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26mi2:35

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I've read (from people that are SpaceX critics Ithink) that the flights so far have carried "payloads" that are below the specs required for effective launches. Is that correct? Does it matter (e.g. that is not what they are trying to accomplish and when it is they will get close to the design requirements)?

Why not use a lowercase v?
 
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kwintsommer

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So...it's just coincidence that the German Nazi's had a V1 and a V2 and this is a V3...right?

It's a version number. Specifically, Version 3. You're reading way too much into it.

If tacking version numbers onto things makes someone a Nazi then I'm guilty and so are an awful lot of engineers and developers. In fact I had an email from a vendor trying to talk me into upgrading to a higher Version this very morning. Maybe I'll write them back accusing them of Nazi sympathies....
 
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For it to be a coincidence, none of the people involved in the decision to use V[number] can have been aware of both the relevant history and the allegations against Musk. That is obviously absurd, which means one of two things is true:
1. They knew and didn't care.
2. They knew and chose it deliberately.

Either way, V[number] isn't a good look when the accusations of Musk being a NAZI were already a thing.

FFS, no one other than the most desperate mental gymnasts is associating the V for version with WW2 Nazi rockets. A stretch to make a joke, maybe, but "isn't a good look"?
 
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Procedural_Username

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It sounds like all of the holds in those final seconds were due to problems with the launch structure and ground systems, not the rocket. It was the same thing with the scrub of Artemis II. I don't understand why ground systems seem to be the source of more scrubs than the rockets, which I would assume are much more complex?

Any system mass that you can move from the vehicle to the ground systems directly improves performance. Any system complexity that you can move from the vehicle to the ground system directly improves reliability and cost, because it is a lot easier to make a cheap reliable system if it doesn't have to be flight weight.

The perfect rocket would be 100% ground system, if your occupants could survive the acceleration and there wasn't so much air at ground level.
 
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Agreed its very difficult to get this all right and safe and working for one launch.

So how is SpaceX going to repeat this 10 - 20 - 50 times in space for any Mars mission ?
Perhaps the company that has built the most reliable, most available and most frequent launch vehicle knows something about improving systems and processes to be repeatable and successful?
 
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SpaceX is a repeat of the Soyuz program and the attempt by the Soviets to try their luck at a moonshot with the N1.

Experience and success at the smaller vehicle does not translate into a formula to build a larger rocket at scale.

How many years and how many re-writes / re-designs has Starship gone thru because the previous was tested and shown to be a failure ?

Even Musk the ultimate grifter knows Starship will n ever work and tahts why he is cashing out.
The most N1-like piece of this rocket - the Super Heavy booster - has actually been the most successful and reliable piece of the architecture to date. The more difficult piece - Starship - is the real wildcard with regard to whether or not this design will successfully achieve full and rapid reuse. But even if full reuse remains out of reach, flying SS/SH in partially reusable mode - like a vastly upscaled Falcon 9 or New Glenn - would still yield unprecedented performance and historically low cost of mass to orbit.
 
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Resistance

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SpaceX is a repeat of the Soyuz program and the attempt by the Soviets to try their luck at a moonshot with the N1.

Experience and success at the smaller vehicle does not translate into a formula to build a larger rocket at scale.

How many years and how many re-writes / re-designs has Starship gone thru because the previous was tested and shown to be a failure ?

Even Musk the ultimate grifter knows Starship will n ever work and tahts why he is cashing out.
Oh please, even someone who hates Musk as much as I do can recognize the realistic assessment that SS is likely to be very successful.
 
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Agreed its very difficult to get this all right and safe and working for one launch.

So how is SpaceX going to repeat this 10 - 20 - 50 times in space for any Mars mission ?
Not so much working for one launch, as working flawlessly for the inaugural launch. There is a huge difference there, but it might be too subtle for you to pick up on...
 
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micktransit

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SpaceX is a repeat of the Soyuz program and the attempt by the Soviets to try their luck at a moonshot with the N1.

Experience and success at the smaller vehicle does not translate into a formula to build a larger rocket at scale.

How many years and how many re-writes / re-designs has Starship gone thru because the previous was tested and shown to be a failure ?

Even Musk the ultimate grifter knows Starship will n ever work and tahts why he is cashing out.
"...Starship will never work..."


That's a bold and confident prediction.

Have you bet a lot of money on it?
Or just your, er, credibility?
 
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The Lurker Beneath

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For it to be a coincidence, none of the people involved in the decision to use V[number] can have been aware of both the relevant history and the allegations against Musk. That is obviously absurd, which means one of two things is true:
1. They knew and didn't care.
2. They knew and chose it deliberately.

Why would anyone who was not deranged care? Vn stands for 'Version N' - a commonly-used construction - and in fact I think SpaceX internally use 'Block N'. The V does not stand for 'Vengeance Weapon', and Starship is not a ballistic war missile.
 
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EllPeaTea

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You also have the deluge system that requires a massive amount of water driven at very high pressures, etc. (actually gas generators built from a set of Raptor derived power heads, rocket engine pressuring the deluge system).
Zach Golden's latest video deals with the design of the new deluge system, and he reckons the new gas generators aren't raptor derived. There's no turbopumps in there at all - it looks to be gaseous O2 and CH4 being fed into a combustion chamber that then warms up a massive flow of N2.

The generators were originally christened "Baby Raptor", but that was before they had any idea of how they worked.
 
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Cold Fussion

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Why would anyone who was not deranged care? Vn stands for 'Version N' - a commonly-used construction - and in fact I think SpaceX internally use 'Block N'. The V does not stand for 'Vengeance Weapon', and Starship is not a ballistic war missile.
That's the thing, it's only deranged people who think this way.
 
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Ooooompf

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Engineers pumped more than 11 million pounds of methane and liquid oxygen into the rocket in less than 40 minutes

I get that 11 million is a large number that reads impressive, but it's also completely meaningless to me and I guess a lot of other readers. Personally I think that 5000 metric tons gives a much better impression of scale. Please and thank you 🙏
 
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mmurray

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It's a version number. Specifically, Version 3. You're reading way too much into it.

If tacking version numbers onto things makes someone a Nazi then I'm guilty and so are an awful lot of engineers and developers. In fact I had an email from a vendor trying to talk me into upgrading to a higher Version this very morning. Maybe I'll write them back accusing them of Nazi sympathies....
Assuming Google AI's extract from the Australian War Memorial is correct:

Germany called the rocket "V-2" because it was the second in their lineup of Vergeltungswaffen (retaliation or vengeance weapons). Originally developed by the German military under the technical designation Aggregat 4 (A-4), the Nazi propaganda machine rebranded it to boost morale and threaten Allied cities

Aggregate seems to mean "unit" in the context of building machinery.
 
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