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Space X CR6 First stage landing

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Re: Space X CR6 First stage landing

#111

Makes me wonder if they just leave them on the ground of the ocean or recover them? ...I bet otherwise the Russians or Chinese would love to get their hands one of them :)

Chinese are just waiting until it succeeds. Their hackers are probably on stand-by to download the blueprints and the code. lol

Re: Space X CR6 First stage landing

#113
post #87

Earlier quoted context omitted.

It burns three times after the second stage detaches. The first is to get the landing zone closer to the takeoff, the second slows it down from 1300 m/s to about 250 m/s, the third slows it to (hopefully) 0 m/s on the landing pad. Here's a diagram: http://media2.s-nbcnews.com/i/newscms/2014_51/812491/141217-... If the 'x-wings' are what I think you're referring to, they're the landing legs. They are shaped like that…

What's the difference between the tests on earth (as seen on youtube etc) where the engine runs the whole time and seems to display good throttle control and this type of landing?

The Grasshopper tests had a full tank of fuel and (if I recall) additional ballast, to counteract the thrust of the engines. That's what allowed them to hover and perform the various low-velocity translation tests.

Of course, these barge landings are the first high-velocity tests, so there'll be kinks to work out.

Re: Space X CR6 First stage landing

#114

It must be amazing working in a field where failure is almost as exciting as success. What's the main obstacle to slowing down and stabilizing the rocket on its descent to the platform? Is it just a matter of speed or also the shape of the rocket and its center of gravity? Would a set of 3 parachutes might slow it down a little bit or at the very least straighten it before the rockets need to kick in saving some fuel…

SpaceX seems to be able to stabilize fine with RCS and/or their grid fins. The rocket design must be reasonably stable--even tail-first.

I don't think incoming velocity is much of a problem. Terminal velocity is gonna be no more than 90 m/s. The engines on that stage are more than capable of slowing it down--and fast. In fact, they're too powerful--it can't hover.

Re: Space X CR6 First stage landing

#115

Why did it explode in such a dramatic fashion? I thought the booster was almost entirely empty when it returns to the barge.

The rocket is, at the very least, a thin pressurized tube full of kerosene vapor and oxygen, and probably some decent amount of liquid kerosene and liquid oxygen. Crack it open and it's gonna make a pretty good flash. But as rocket explosions go, that wasn't very big. Get to YouTube if you want to see some real rocket explosions.

Re: Space X CR6 First stage landing

#116

Earlier quoted context omitted.

Watching it made me realize I only had an abstract idea of how difficult it was to even attempt this. It's insanely hard, and they're so close!

Yes its a very hard problem but what makes it hard ? Is it engineering of the components, algorithms or expensive tests and economics of it ? Maybe people before Elon Musk were not interested in solving this problem not because its technically hard problem but because their existing business model is much more lucrative.

You have to deal with real physics and the real physical world - turbulence, friction, lag, wind, waves, none of which are predictable.

Re: Space X CR6 First stage landing

#117
Is there a reason you couldn't have things on the side of the landing pad that "grab" onto it and secure it?

It could be as simple as a huge ring of cable that just closes around the top of the rocket, then pulls it tight on all sides- like the guidelines on a tower to keep it stable.

Maybe they don't want to do that because they think they can do it without it?

Re: Space X CR6 First stage landing

#118
Pretty inspiring after all this time that the problem is not so much getting stuff up, but landing it successfully. I kind of feel like this is where we should have been in the 70s.

Re: Space X CR6 First stage landing

#119
post #61

I wonder what happened there. Looks at 4 seconds the guidance system figured it needed to pull an ultra manoeuvre to slow the the horizontal speed(was drifting left) but ended up with a solution putting the rocket upright again at nearly 0m. If it would have left some altitude for stabilizing I think they would have had it. Arm chair rocket science is fun.

As mentioned, it's control system lag, which led to over-correction oscillations. This is very straightforward to deal with.

Re: Space X CR6 First stage landing

#120
post #113

Earlier quoted context omitted.

What's the difference between the tests on earth (as seen on youtube etc) where the engine runs the whole time and seems to display good throttle control and this type of landing?

The Grasshopper tests had a full tank of fuel and (if I recall) additional ballast, to counteract the thrust of the engines. That's what allowed them to hover and perform the various low-velocity translation tests. Of course, these barge landings are the first high-velocity tests, so there'll be kinks to work out.

Thanks, that would explain that.

I was impressed by how small the barge looked compared with the F9 it's clever that the F9 can autonomously target such a small area. If they keep targeting 'Just Read the Instructions' by the time land based landings come to be it will be nailed. Awesome stuff!

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