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#161 |
Fiend God
Join Date: Oct 2005
Location: In a post-fact world
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What's got you confused? I'm saying that so long as the project focuses on precise goals, and thus fewer flights, they can insure that launches are safe for the crew. If and when it becomes commercial, that might no longer be true. Launching rockets is inherently dangerous; much more so than with planes.
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#163 |
Fiend God
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#164 |
Pi
Join Date: Nov 2005
Posts: 21,734
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Because you started with this:
Note the 'if' at the beginning there. There is no 'if' there That's exactly what he's trying to do now, with this project and this tech, right now. That's why I'm so confused. You say you have a handle on what he's doing, but you, at the same time seem to think he's not doing that. Musk is currently trying to impliment routine orbital flights. You seem to think there's an 'if' in that statement. There isn't. But you also tell me you know what he's doing. |
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#165 |
Fiend God
Join Date: Oct 2005
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Yes but that doesn't mean he'll succeed. I hope he does, but there are giant hurdles to clear from here to there. He may realise that before getting to that point, and abandon the project, focusing on more 'classic' operations. Hence the 'if'. At this point I think we're several steps behind that.
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#166 |
Pi
Join Date: Nov 2005
Posts: 21,734
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No, it doesn't, but that's not what you said.
You said: "Sure, if Musk ever comes around to try to implement routine orbital flights" Which is just in opposition to reality as that's exactly what he's trying to do. There's no 'if' in that sentence if you want it to match what's Musk is actually doing, which is: Trying to implement routine orbital flights. Perhaps you can't see why your statement is so confusing. Perhaps I'm banging my head against a brick wall. Perhaps I'm going to take an asprin and have a lie down. Who knows. |
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#167 |
Guest
Join Date: Apr 2004
Posts: 29,033
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They also had a single landing incident, and one incident where people died in a test that was never intended to fly. I think the Russians have had only one fatal accident.
Four incidents with fatalities isn't huge, considering the nature of the endeavor, but for consumer use, it's kind of extreme. Commercial flights will need to have a much better track record than NASA has had if they want to be commonplace. ETA: I just looked it up. 553 people have made it into Earth orbit. 21 have died in space related accidents. Before space flight becomes "routine", Musk et. al. will have to do a lot better. |
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#168 |
Fiend God
Join Date: Oct 2005
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That's what he's planning to do, once the technology is sufficiently developed. But correct me if I'm wrong, the Starship is supposed to serve other missions as well such as a Mars mission, which certainly isn't routine anywhere in the near future. Some of the goals of the design might be pursued, and others not. We're not there yet. Right now we're trying to make the damned thing work.
I don't know why it was necessary for you to get personal, considering how trivial of a disagreement this is. |
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#169 |
Fiend God
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#170 |
Pi
Join Date: Nov 2005
Posts: 21,734
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It pretty much is. It would take six consecutive flights to refuel a Starship to get it to Mars. Currently planned to be one after the other in rapid succession. The Mars plan absolutely needs the launches to be routine.
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I'm going to go and have that lie down now. |
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#171 |
Fiend God
Join Date: Oct 2005
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Ok maybe we're just disagreeing on what 'routine' means. I don't mean 'routine' like a shuttle launch. I mean 'routine' like a 777 takeoff.
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#173 |
Penultimate Amazing
Join Date: Nov 2006
Posts: 14,185
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I think he is simply saying that there is no reason they can't match NASA's safety record. As long as SpaceX is in the same of mode of limited flights, no need to consider an accident a given as opposed to a potentiality. The "one in a million" comparison to airliners isn't relevant until SpaceX is flying on the scale of airliners.
ETA: Sorry, I hadn't noticed the conversation went on to another page beyond the post I replied to. |
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#174 |
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#175 |
Fiend God
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#177 |
Fiend God
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#178 |
Penultimate Amazing
Join Date: Oct 2012
Location: Nelson, New Zealand
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Two during space operations
24 April 1967: The astronaut aboard Soyuz 1m Vladimir Komarov dies when his parachute failed 30 June 1971: The crew of Soyuz 11, Georgy Dobrovolsky, Viktor Patsayev and Vladislav Volkov, died from lack of oxygen after a cabin vent valve opened during separation from the Salyut 1 space station They also had numerous other fatal accidents including the massive explosion of a Vostok rocket that killed 48 people in 1980, and the earlier Nedelin Disaster in October 1960 where the second stage of an R-16 rocket ignited on the launch pad killing up to 300. |
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#179 |
Fiend God
Join Date: Oct 2005
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Let's just say that 'soviet' wasn't much of a seal of quality.
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#180 |
Pi
Join Date: Nov 2005
Posts: 21,734
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They were pretty good at innovation though. And their safety record probably compares quite well with the US one due to the two shuttle disasters. (not entirely sure about that though) They also made full-flow staged combustion when the US had, I think, deemed them impossible. And Soyuz was the only game in human rated spaceflight for years The N1, however, was a very, very expensive firework. ![]() |
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#181 |
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#182 |
Fiend God
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#183 |
Loggerheaded, earth-vexing fustilarian
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#184 |
Fiend God
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#185 |
Penultimate Amazing
Join Date: Feb 2005
Location: Shanghai
Posts: 15,513
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Thanks!
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Quote:
But I definitely agree that everyone at SpaceX would have been a lot happier with an unmitigated success and no explosion. I would too! ![]() I'm only saying that incremental progress is still progress, and as far as I can tell it seems like they're progressing about as fast as they expected to. I think the people at SpaceX out to be pretty happy about that, given the difficulty of what they're trying to achieve. |
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#186 |
Penultimate Amazing
Join Date: Feb 2005
Location: Shanghai
Posts: 15,513
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That's a good point. The difficultly of launching rockets safely enough for commercial passenger flights is pretty high, but landing them again in the way SpaceX does at least seems to be even harder.
Not to say they can't achieve it, but yeah it's a very difficult undertaking. One thing that I think will help is if they can get enough rockets flying for other purposes first to really work out the issues with it. If you're launching hundreds of times/year (without passengers), you have plenty of chances to find the problems that might come up and fix them. |
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"... when people thought the Earth was flat, they were wrong. When people thought the Earth was spherical they were wrong. But if you think that thinking the Earth is spherical is just as wrong as thinking the Earth is flat, then your view is wronger than both of them put together." Isaac Asimov |
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#187 |
Fiend God
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#188 |
Penultimate Amazing
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Those who claim that something can't be done need to stop getting in the way of those who are actually doing it! - Anonymous Its TRE45ON season... convict the F45CIST!! |
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#189 |
Penultimate Amazing
Join Date: Nov 2006
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#190 |
Penultimate Amazing
Join Date: Feb 2005
Location: Shanghai
Posts: 15,513
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Isn't that the plan with Starship? Or is the idea still that Starship would launch with a Dragon capsule as payload which can then do reentry on its own?
That probably does make more sense, and even if it's not the plan now, it could be done that way if landing can't be made reliable enough for human safety. (I apologize for not looking this up myself, my VPN subscription expired and I've yet to renew it, which means I'm currently stuck behind the Chinese firewall, so no google, or wikipedia...) |
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"... when people thought the Earth was flat, they were wrong. When people thought the Earth was spherical they were wrong. But if you think that thinking the Earth is spherical is just as wrong as thinking the Earth is flat, then your view is wronger than both of them put together." Isaac Asimov |
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#191 |
Penultimate Amazing
Join Date: Nov 2006
Posts: 14,185
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Other than the Dragon capsule, I'm not sure of the details of what they have in mind for passengers.
I haven't been paying enough attention to this recently, so let me ask some stupid questions. SN10 was a test of the first stage, correct? I think there are only 3 Raptor engines in this vehicle and I think the full two stage configuration would have six. This was testing the recovery of the first stage, wasn't it? If this had been a real flight the passengers would have been on the second or third stage and it wouldn't matter that their first stage had exploded long after they were done with it. |
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#192 |
Philosopher
Join Date: Jul 2011
Location: Colorado
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#193 |
Penultimate Amazing
Join Date: Oct 2012
Location: Nelson, New Zealand
Posts: 24,829
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No, SN10 is not even remotely like any of the Starship stages, although it looks similar in shape to what the second stage is expected to look like. (The first stage is the superheavy booster, which will re-enter and land in much the same way as the Falcon 9 booster - tail first, with an "entry burn" and a "landing burn")
SN10 is a test article, nothing more. It has much the same sort of role that the SpaceX "Grasshopper" had, i.e. proving the concept that autonomously hovering and landing a rocket at a precise location was feasible. It is purely for testing the concept of free-falling towards a landing in which the second stage will flip from near horizontal to vertical, as we saw it doing. The reason for this is that the intention is for the Starship second stage to re-enter from orbit in that nose-up belly first attitude, shedding off orbital velocity until comes down to terminal velocity. The reason for the two different methods is simple... the first stage only has to re-enter at speeds of around 6,000 kph - that is relatively low, so the engine bells and associated structure do not have to withstand a great amount of heating - the reason for the entry burn is to shed off speed to limit that heating. However, the second stage will be entering the earth's atmosphere at orbital velocity, about 28,000 kph - no entry burn, and the kicker is that convective heating isn't just proportional to velocity, its not even velocity squared, its velocity cubed!! - so double the entry speed from 6,000 to 12,000 kph, and the heating effect is eight times greater than at 6,000, double it again to 24,000 kph and the heating effect is 64 times greater than at 6,000 kph*. Obviously, the thrust structure would not be able to withstand this; any attempt to re-enter tail first at those speed would result in the destruction of the vehicle. SpaceX had to come up with a different way to re-enter and land the second stage. * This is the simplified version. There is also radiative heating that needs to be considered, and it is proportional to the eighth power of velocity. |
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Those who claim that something can't be done need to stop getting in the way of those who are actually doing it! - Anonymous Its TRE45ON season... convict the F45CIST!! |
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#194 |
Loggerheaded, earth-vexing fustilarian
Join Date: Sep 2006
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SN8/9/10 have all experienced disaster at or just after landing. In addition, launch technology is well established, while soft landings are novel. Musk said, of this very technology, something like "There will be some holes in the ground along the way", and he wasn't talking about launches.
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#195 |
Penultimate Amazing
Join Date: Oct 2012
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Those who claim that something can't be done need to stop getting in the way of those who are actually doing it! - Anonymous Its TRE45ON season... convict the F45CIST!! |
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#196 |
Fiend God
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#197 |
Fiend God
Join Date: Oct 2005
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Anyway we need to rename the thread to "Starship Blew Hop".
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#198 |
Penultimate Amazing
Join Date: Nov 2006
Posts: 14,185
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Thanks crescent and smartcooky.
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#199 |
Penultimate Amazing
Join Date: Nov 2006
Posts: 14,185
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Just guessing, but in normal operations it probably detaches before the orbit is circularized so it's orbit still intersects the atmosphere. And probably pretty close to intersecting the surface of the Earth.
ETA: No, on reading the Wikipedia the current plan is for the second stage to make orbit, so I'm confused about the no burn comment too. |
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