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Starship Integrated Flight Test 2 at 7 Am Central Time

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Re: Starship Integrated Flight Test 2 at 7 Am Central Time

#371
post #277

Earlier quoted context omitted.

Small correction, I think. The booster appeared to survive hot staging fine. It went through quite a bit of it's flip back maneuver. It was awesome to watch. There were some interesting activations of engines in the booster engine ring at that point. It's unclear to me if that was anticipated as an offset subset was what was desired for the off axis maneuver, or things were degrading at that point. And then it blowed…

Watching the replay, it looks like some of the engines failed to light during boostback reignition. Then, either total flameout occurred, or AFTS started cutting fuel in preparation for termination (maybe there are settings for "terminate right tf now" and "try to shut down engines before popping off", idk just speculating). Either way, it looks like the start of boostback was not quite norminal, and AFTS decided tha…

All but one engine successfully relit (the outer engine ring has no re-light capability) but they started to fail quickly afterwards.

Scott Manley also has the theory that the maneuver caused a sloshing motion of the fuel and the water hammer ruptured piping on the engines, causing a cascading failure.

https://www.youtube.com/shorts/7LYw6gU65ac

Re: Starship Integrated Flight Test 2 at 7 Am Central Time

#372

- Starship got just below orbit - Booster destroyed during hot staging - SpaceX reporting that destruct system fired on upper stage towards end of burn all in all a pretty good result: clean launch and separation, good performance on the booster during ascent (no engine mishaps this time)

Wonder if hot staging caused issues with both vehicles or it was two separate issues.

The booster experienced a rapid unscheduled disassembly after boostback burn following the successful stage separation

Re: Starship Integrated Flight Test 2 at 7 Am Central Time

#373
post #358

Earlier quoted context omitted.

It's good enough for NASA. https://www.nasa.gov/centers-and-facilities/white-sands/dest... We've crashed production probes into Mars, we've burned astronauts alive, we've had the supposedly "safe" options like Boeing's Starliner have fundamental problems even making it to orbit. Space has always been this way. Starship's more akin to taking the Bell X-1 up for a spin than flying a 787 around, for the time being. Prob…

This is a false dichotomy. On one side we are talking about how the "space industry" is most moving slowly and how spacex is doing great things. On the other side we are saying that this is good enough for nasa (who is the establishment when it comes to space) and yolo bro. On one side we are defending nasa because priorities, but on the other side we're cheering on spacex who is ultimately sucking at the big fat gov…

I don't know why you're being a contrarian here. Booster completed it's primary mission. Main vehicle survived long enough to show viability. Multiple technologies were proven beyond a reasonable doubt to work.

Shuttle was 1.6 billion a launch. This is gonna be 100 million a lunch even if you let the booster blow up every time.

This test is in line with how every new rocket is developed. You really need to Google the 50s and 60s of space flight and see how many rockets were lost in those days.

Yet they still got to the moon.

Re: Starship Integrated Flight Test 2 at 7 Am Central Time

#374

Earlier quoted context omitted.

Space Shuttle didn't have an escape system either; its total death toll was 14.

Absolute numbers don’t really mean much. More than 14 people have died since this test flight on American roads. Shuttle death rate was about 1 in 75, which is insanely high.

How does that compare with other rocket systems?

Re: Starship Integrated Flight Test 2 at 7 Am Central Time

#375

Earlier quoted context omitted.

Starship didn't really start in a meaningful way in 2012. In 2012 there were at best some vague concepts of a large rocket and some initial concept ideas for Raptor. But at that time for Raptor they were still thinking about Hydrolox. SpaceX simply didn't have the resource to fully invest in Starship until much later. Even by the early presentations around 2016 it was a tiny part of SpaceX and was prototyping with li…

Well, whether you want to call it 8/9 years ('61-'69) or 14 ('55-'69), I don't think NASA looks too shabby landing men on the moon in that time frame without the decades of experience we have to draw on today, and with 1950's/60's technology, and so far no-one else has done it.

The NASA of that time has been long gone for decades

Re: Starship Integrated Flight Test 2 at 7 Am Central Time

#376
post #265

Earlier quoted context omitted.

Couldn’t Starship detach and fire its engines to get away from the booster? Of course I guess if they are not hypergolic there is startup time.

The real question here is what happens with a crewed second stage that has a problem with its engines/fuel. We’ve yet to see designs for the crewed interior beyond very conceptual stuff. Maybe something like https://en.wikipedia.org/wiki/Escape_crew_capsule for launch abort.

How did Space Shuttle approach this problem?

Re: Starship Integrated Flight Test 2 at 7 Am Central Time

#377
post #374

Earlier quoted context omitted.

Absolute numbers don’t really mean much. More than 14 people have died since this test flight on American roads. Shuttle death rate was about 1 in 75, which is insanely high.

How does that compare with other rocket systems?

Pretty poorly, Soyuz has 4 fatalities (Soyuz 1, Soyuz 11) during it's over 140 flights, Crew Dragon has none.

Re: Starship Integrated Flight Test 2 at 7 Am Central Time

#378
post #370

Earlier quoted context omitted.

At this altitude, the vehicle is pretty much in the vacuum and grid fins have absolutely no control authority. It could have resulted in failure later on but not at that point where the booster blew up.

Saw that Scott Manley video that came out right after that and it looks like fuel issues to engines probably caused it. All but one engine started up, but they started failing after that. https://www.youtube.com/shorts/7LYw6gU65ac

Then it's not hot staging but maybe sloshing of fuel in the tank just simply.

Re: Starship Integrated Flight Test 2 at 7 Am Central Time

#379

Earlier quoted context omitted.

The real question here is what happens with a crewed second stage that has a problem with its engines/fuel. We’ve yet to see designs for the crewed interior beyond very conceptual stuff. Maybe something like https://en.wikipedia.org/wiki/Escape_crew_capsule for launch abort.

This same question was asked in the early years of commercial aviation. In the end, the industry (mostly) settled on aircraft designs that could passively glide reasonably well enough to land (sometimes). But some aircraft, e.g. military jets and Cirrus, came up with different answers (parachutes for the crew and for the whole aircraft, mostly). We'll see how the commercial spacecraft industry deals with this, but I…

Wonder if we'll ever have commercial aircrafts with whole aircraft parachutes.

Re: Starship Integrated Flight Test 2 at 7 Am Central Time

#380
post #87

Earlier quoted context omitted.

Why so long? Will they need to go through another round of FAA approval? Or?

They need to redesign the bottom half of the rocket so it doesn't blow up during staging, and figure out what happened to the top half and fix that.

Complete nonsense. Which anyone with even cursory interest in Starship's development can confirm.
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