Відео

This looks pretty dramatic but remember spacex is trying to find the bare mimimum. If nasa were building this it would cost 10x as much and take up 100x the area. Think 39a (built for saturn V) but 2.5 times bigger.

fyi: cant wait for the new video!

would be more enjoyable with out the attempted commentary

If the Chinese can watch every single video of csi starbase I swear they'll have more information to create a replica of the starship

Hey, would you use your fame and starpower to set up a skydiver with a clear lexan tube about 5% full of liquid and jump out of a plane maybe 10,000 feet up and train cameras on the fluid? This might give some insight into the problems faced in relighting the engines on starship.

Hey @CSIStarbase, could you do poster/prints of the Starship Family Tree shown at 13:55 ? Be sick to have that on my wall.

Simply Love this man ..

You guys are amazing and figuring stuff out

My dude. Amazing video. The sound is excellent - just everything is so well done. What a pleasure to watch, thank you.

Zach! Such good content! Thank you for your hard work!

Wow! Finally finished this amazing video. Thank you for all your - and everyone's - hard work putting this together for us.

Aerospace Coffeezilla 😂😂❤❤

Need a different system for the "lifting rig" to lift Starship. Too much damage to tiles.

Wow amazing zach one of the koolest guys in space related things. you tim dodd and felix are my three favourites. Now i finally know why ship 20 and booster 4 didnt fly good thing they didnt too.

Wow this is the best video of yours i have seen yet. Keep up the good work was interesting to see starships development right from the start thanks.

that video was worth the watch alone for tim dodd everyday astronaut section lol not to mention the great details. good job stage zero zack

It seems that propellant/oxydizer tanks which are static and allow he liquid to freely move around is simply a design error that should be fixed. If a container for these liquids could be designed that shrinks in volume at the same rate as the volume of liquid is decreasing, keeping the liquid pressure constant, this would eliminate the problem. One way of doing that would be to inflate an elastic bag filled with inert gas (helium for instance) to compensate for th amount of liquid consumed from the tank.

Only about half-way through this because is has so much detail and excellent information and watching after IFT-3. Could the Hot Stage ring been damaged and affected the booster grid fins/electronics? Might it help if an ablative shield or TPS tiles were placed at least on some of the dome? Thank you again for an amazing job on this video. Really well done.

Great presentation and you do an exemplary delivery. Thank you.

Hot staging is not radical at all. It is very effective at providing extra lift: an extra approximately 18%.

Such a wealth of knowledge. Incredible graphics and spot on narration. Bravo!

Would you really go to Mars, Zack ???

Awesome work!😄😃

I wanted to hear the motor engines, not some morons screaming.

I came to hear a rocket launching…. I heard a Québécois and a giant popcorn machine on steroids 😂 An incredible sound hard to forget, well captured. Congrats to everyone at SpaceX!

This data is 2 levels above! Why don't more subscribe?

Separate from booster with retro braking/boosting then fire the vac engines far away from booster?

very informative, thank you! ❤

You were right about the grid fin actuation before hot staging, you can see it on the onboard footage.

Great youe selling gendered products how wonderful

That is actually the best channel about Starship that exists, I value all the details you put in and spend the time researching! I can't wait to see the IFT-3 analysis, no matter if released in a week or more than a month, I have no doubt it will be very informative!

Every launch has more success than the previous one and all the while they are gathering data. Loss of data is by far the most serious failure because it loses the detail that defines the problem and the solution. It's called DOE for Deign Of Experiments. Every attempt is an experiment which yields more data and more solutions.

An excellent record, thanks for posting!

after ift3 the staggered rvac ignition theory doesnt hold, gridfins do

New sub. This channel is next level. Thank you for all your research, and hard work. I learned a lot. Love your work.

So, assuming both fuels remain liquid, why don't these tanks have baffles in them to keep the fuel from moving around inside the tanks? More to the point, if they're worried about the fuel rapidly moving to the opposite end of the tank, why don't they have something like a disc that will travel down the tanks as the fuel is consumed to minimize the amount of empty space that the fuel has to move around in? Either that or install a bladder that will compress as the fuel leaves the tank. Either would be a good option to keep this from happening again on future launches. I'm sure they'll figure that out eventually.

After seeing IFT 3 (particularly at T +2'37), your hypothesis that the fins help to rotate the booster seems to be right!

viendo esto antes del IFT3 me siguen dando escalofrios de felicidad al ver esto, igual que cuando lo vi en vivo.

12:04 the music is so good and loud I have a hard time understanding the explanation! But otherwise very cool video, thanks for sharing <3

As a layman i told mr x use hourglass tanks closing the bottleneck as the uppers become empty. Best part no part less baffling parts.

It just sounds like a shooting 😭

Thanks men i learned a lot. I was always thinking why the quick turn around with the hot stage? that would cause the fuel to rock arround in the the tank and destroy the inside. Thank's and Greetings from Holland

It would be cool of the first payload was a cyber truck 💥💥💥

Probably need reverse boosters to pull the sections apart you put the reverse boosters on the side ignite them when you want to separate from one stage

1:00:41 These animations are getting so realistic its hard to tell them apart from real life.

The effort put into this video is absolutely ridiculous

They don’t have SpaceX engineers running for the hills over nothing they already said the staging wasn’t the problem. They found the problem like a week ago and posted it up to multiple sources so you need to update your video. It’s not the staging. It was not the thrust that caused the problem, but if you actually listen to SpaceX engineers and SpaceX channels, you would know this

During the heat shield testing, think of creating a pressure differential instead of changing the absolute pressure.

Does the mass of the inner stage mostly cancel out the gains of hot staging? What is the new lift number after subtracting the inner stage?