Author Topic: First stage recovery at down-range locations  (Read 175086 times)

Offline mlindner

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Re: First stage recovery at down-range locations
« Reply #20 on: 03/27/2013 02:21 am »
Make note here. Landing on a hard vessel deck is _worse_ than landing on land. If you catch a boat on an upswing your impact speeds are even worse than landing on land. If you're going to land on a hard surface anyway, just land on land.
« Last Edit: 03/27/2013 02:22 am by mlindner »
LEO is the ocean, not an island (let alone a continent). We create cruise liners to ride the oceans, not artificial islands in the middle of them. We need a physical place, which has physical resources, to make our future out there.

Offline RobLynn

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Re: First stage recovery at down-range locations
« Reply #21 on: 03/27/2013 04:44 am »
A really big catamaran would be easy and cheap to do, say 100mx100m would only cost a few millions (100m barges cost as little as 2-3million) and could travel downwind on a pre-programmed path to reduce effect of waves and wind - potential for reduced impact of cross winds is actually an advantage over land based landing.

If the rocket came in to a hover at a few meters altitude then a fixed grappling hook on top of the rocket could be caught by a wire that swept across at the right altitude, eliminating landing legs, and making it impervious to cross winds.  An oversized digger could just about do the job.  Simpler still the rocket could just translate itself laterally to hit a horizontal catch wire (their guidance systems are obviously capable).  If such a manoeuvre can be done with only 5-10 seconds of additional thrust then it is probably cheaper than landing legs, and the system could be easily transferred to a ship or other relatively unprepared landing site.
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Offline Jason1701

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Re: First stage recovery at down-range locations
« Reply #22 on: 03/27/2013 05:10 am »
A really big catamaran would be easy and cheap to do, say 100mx100m would only cost a few millions (100m barges cost as little as 2-3million) and could travel downwind on a pre-programmed path to reduce effect of waves and wind - potential for reduced impact of cross winds is actually an advantage over land based landing.

If the rocket came in to a hover at a few meters altitude then a fixed grappling hook on top of the rocket could be caught by a wire that swept across at the right altitude, eliminating landing legs, and making it impervious to cross winds.  An oversized digger could just about do the job.  Simpler still the rocket could just translate itself laterally to hit a horizontal catch wire (their guidance systems are obviously capable).  If such a manoeuvre can be done with only 5-10 seconds of additional thrust then it is probably cheaper than landing legs, and the system could be easily transferred to a ship or other relatively unprepared landing site.

The vehicle will have too much thrust to translate horizontally.

Offline RobLynn

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Re: First stage recovery at down-range locations
« Reply #23 on: 03/27/2013 06:57 am »
A really big catamaran would be easy and cheap to do, say 100mx100m would only cost a few millions (100m barges cost as little as 2-3million) and could travel downwind on a pre-programmed path to reduce effect of waves and wind - potential for reduced impact of cross winds is actually an advantage over land based landing.

If the rocket came in to a hover at a few meters altitude then a fixed grappling hook on top of the rocket could be caught by a wire that swept across at the right altitude, eliminating landing legs, and making it impervious to cross winds.  An oversized digger could just about do the job.  Simpler still the rocket could just translate itself laterally to hit a horizontal catch wire (their guidance systems are obviously capable).  If such a manoeuvre can be done with only 5-10 seconds of additional thrust then it is probably cheaper than landing legs, and the system could be easily transferred to a ship or other relatively unprepared landing site.

The vehicle will have too much thrust to translate horizontally.

Interesting, by that do you mean that it will be decelerating at 2+ g (Merlin 1D 450kN minimum thrust at 70% throttle, <20tonne landed weight) and so can only manage a parabolic ground-kissing trajectory?

That would give only about 2seconds below 5m, which would be very tough for a catcher system.  Would also mean that couldn't run engine during much of descent - only around 10s of motor firing in the terminal descent to landing phase which could make terminal guidance very difficult unless they do multiple restarts during descent.  Can't wait to see what future grass-hopper tests look like if they are flying similar profiles.

For the curious the Ryan X13 Vertijet from the 50's was a vtol jet with a nose mounted catcher system, check out 12:30:
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Offline VatTas

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Re: First stage recovery at down-range locations
« Reply #24 on: 03/27/2013 08:18 am »
Oh no, not again. Hooks and cables...

Offline mlindner

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Re: First stage recovery at down-range locations
« Reply #25 on: 03/27/2013 08:30 am »
Oh no, not again. Hooks and cables...

Indeed. I think this is the third time in the last 2 months this has been brought up.

RobLynn. Go read here and the reasons it was shot down. http://forum.nasaspaceflight.com/index.php?topic=30350.msg1000045#msg1000045

Edit: I'm new to the huge history of random tests the military and NASA have done in ages past. But why does it seem like every other day someone comes around and says "Look look! They had a test program for it in the past so it must be a good idea to try again!"? This keeps happening.
« Last Edit: 03/27/2013 08:32 am by mlindner »
LEO is the ocean, not an island (let alone a continent). We create cruise liners to ride the oceans, not artificial islands in the middle of them. We need a physical place, which has physical resources, to make our future out there.

Offline MP99

Re: First stage recovery at down-range locations
« Reply #26 on: 03/27/2013 11:33 am »
Oh no, not again. Hooks and cables...

Indeed. I think this is the third time in the last 2 months this has been brought up.

RobLynn. Go read here and the reasons it was shot down. http://forum.nasaspaceflight.com/index.php?topic=30350.msg1000045#msg1000045

Edit: I'm new to the huge history of random tests the military and NASA have done in ages past. But why does it seem like every other day someone comes around and says "Look look! They had a test program for it in the past so it must be a good idea to try again!"? This keeps happening.

Lots of tests on video phones back then, too.

Today the technology is ready for Skype. (And cube sats!)  ;D

Some things that were before their time then are feasible now.

Cheers, Martin

Online meekGee

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Re: First stage recovery at down-range locations
« Reply #27 on: 03/27/2013 06:21 pm »
For the curious the Ryan X13 Vertijet from the 50's was a vtol jet with a nose mounted catcher system, check out 12:30:


For the record:
1:  Gulp.
2:  The test pilot is insane.  The guy in the tower with the catch hook and wire escape system is insane.  The guys walking the tarmac around the back to get a better view of the "landing" are insane. 
3:  This kind of ballsy engineering and risk taking is exceptional and sourly missed today. This is why people see SpaceX as different, though clearly not half as ballsy as these guys...   which is a sad statement about the times.
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Offline llanitedave

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Re: First stage recovery at down-range locations
« Reply #28 on: 03/27/2013 06:26 pm »
which is a sad statement about the times.

No, it's a good statement.  We don't need to lose talented engineers by taking stupid risks.
"I've just abducted an alien -- now what?"

Offline douglas100

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Re: First stage recovery at down-range locations
« Reply #29 on: 03/27/2013 07:24 pm »
Using landing legs its better. It gives a better margin for a safe landing if there is an error, or a gust of wind or something. It's also a lot simpler. Everything is a trade. You are already accepting you will lose payload performance when you recover a stage. I think it is much better to accept the extra mass of the landing gear in return for increased assurance of a safe landing. This is about reducing costs, not who comes up with the most complex original idea. A stage which misses the catcher and crashes is worth nothing to anybody.
« Last Edit: 03/28/2013 09:08 pm by douglas100 »
Douglas Clark

Offline R7

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Re: First stage recovery at down-range locations
« Reply #30 on: 03/27/2013 07:36 pm »
A really big catamaran would be easy and cheap to do, say 100mx100m would only cost a few millions (100m barges cost as little as 2-3million) and could travel downwind on a pre-programmed path to reduce effect of waves and wind - potential for reduced impact of cross winds is actually an advantage over land based landing.

Is there still danger that Bezos might actually get a patent for landing a rocket on a sea installation?
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Offline MP99

Re: First stage recovery at down-range locations
« Reply #31 on: 03/27/2013 08:07 pm »


Oh no, not again. Hooks and cables...

Some things that were before their time then are feasible now.

Cheers, Martin

Just because it's feasible doesn't mean it's a good idea. Using landing legs its better. It gives a better margin for a safe landing if there is an error, or a gust of wind or something. It's also a lot simpler. Everything is a trade. You are already accepting you will lose payload performance when you recover a stage. I think it is much better to accept the extra mass of the landing gear in return for increased assurance of a safe landing. This is about reducing costs, not who comes up with the most complex original idea. A stage which misses the catcher and crashes is worth nothing to anybody.

How can I respond to that when you cut out the comment I was actually responding to??

cheers, Martin

Offline douglas100

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Re: First stage recovery at down-range locations
« Reply #32 on: 03/27/2013 09:32 pm »
Sorry, I cut it to save space. What comment were you actually responding to?
Douglas Clark

Offline Avron

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Re: First stage recovery at down-range locations
« Reply #33 on: 03/27/2013 10:40 pm »
1) I just don't see how down range will work.. once you are there if you can make it you need an army and equipment and logistics to get it back to the factory or Pad area.. I cannot see where the savings will be in reuse when you need so much logistics .

2) Once you have boosted yourself downrange your velocity may not be any better than when you started, so you need to turn the stage around to slow down horizontally .. how are you going to turn the stage around.. remember is busy falling into thicker air going downhill.

I don't see downrange as a return to launch site as an option..


Online meekGee

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Re: First stage recovery at down-range locations
« Reply #34 on: 03/27/2013 11:06 pm »
which is a sad statement about the times.

No, it's a good statement.  We don't need to lose talented engineers by taking stupid risks.

There is a sweet spot between taking crazy stupid risks, and between being so risk averse that we're even fearful of development failure (as opposed to accidents), CYA rules the day, and the biggest selling point of a proposal is how non-revolutionary it is and how much it "re-uses existing proven hardware".

SpaceX did not make a person drive GH first-hand, right?  The cowboy was just a joke, and Dragon-cargo is being tested ahead of Dragon-people.  Time are different now in some good ways too.

But SpaceX is NOT afraid of development failure, has no issue with going back to basics and engineering things from scratch, even if people have to sign their names next to projects that might fail. It's a cultural thing, is led from the top, and is nice to watch.
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Offline Ludus

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Re: First stage recovery at down-range locations
« Reply #35 on: 03/27/2013 11:17 pm »
1) I just don't see how down range will work.. once you are there if you can make it you need an army and equipment and logistics to get it back to the factory or Pad area.. I cannot see where the savings will be in reuse when you need so much logistics .

2) Once you have boosted yourself downrange your velocity may not be any better than when you started, so you need to turn the stage around to slow down horizontally .. how are you going to turn the stage around.. remember is busy falling into thicker air going downhill.

I don't see downrange as a return to launch site as an option..



From everything Musk has said, he won't be satisfied with anything short of it flying back to the pad and landing itself. On the way there though I could see them trying landings at sea even with expendable first stage cores, no landing gear, no barge . They could learn a lot from relighting and partial recovery. Obviously that's out at sea. A barge out there and landing a version with folding legs would make sense as an intermediate effort before trying to bring it back to a populated area.

Offline llanitedave

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Re: First stage recovery at down-range locations
« Reply #36 on: 03/28/2013 12:04 am »
which is a sad statement about the times.

No, it's a good statement.  We don't need to lose talented engineers by taking stupid risks.

There is a sweet spot between taking crazy stupid risks, and between being so risk averse that we're even fearful of development failure (as opposed to accidents), CYA rules the day, and the biggest selling point of a proposal is how non-revolutionary it is and how much it "re-uses existing proven hardware".

SpaceX did not make a person drive GH first-hand, right?  The cowboy was just a joke, and Dragon-cargo is being tested ahead of Dragon-people.  Time are different now in some good ways too.

But SpaceX is NOT afraid of development failure, has no issue with going back to basics and engineering things from scratch, even if people have to sign their names next to projects that might fail. It's a cultural thing, is led from the top, and is nice to watch.

I'm not saying Space X is taking stupid risks.  Looks to me like they're taking a conservative approach to testing while still being innovative.  Seems smart to me.

I've spent more than 25 years in an industry that's not known to be particularly safe (drilling and mining), and I know what things were like in the old days, before management could care two whits about either safety or environmental protection.  We're all still paying for some of that attitude.  Miner's deaths used to be not worth mentioning, now they're major news and cautionary examples.  Needless to say, since OSHA and MSHA seeped into the culture of the industry (and it's still not completely there within some companies I wouldn't want to work for) deaths and injuries have gone way down, and environmental catastrophes have declined tremendously -- yet at the same time mining is more productive and efficient than ever before.  Those two facts are not unrelated.  The technology of mining has seen great innovation, in large part because of the requirement to protect human safety and the surrounding environment. 
Yes, mining is more expensive now, but the lives of miners are no longer as cheap, either.  It's more than worth the tradeoff.

This attitude can and should (and apparently does) apply to human spaceflight as well.  As stupendous and inspirational as Apollo was, it was extremely dangerous, and it was in large part a matter of luck that we didn't lose more astronauts and ground crew than we did.  Accidents like Challenger and Columbia are no longer acceptable, nor should they be.  We have to accept some risk, but we should always be pushing at the envelope of safety as well as capability.  Whatever you might like or not like about SLS, I think it's a step forward in that respect, and I'm hopeful that Space X is following that same path.  They have to, if the goal of making space accessible to all is ever to be achieved.
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Online meekGee

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Re: First stage recovery at down-range locations
« Reply #37 on: 03/28/2013 12:27 am »
I've spent more than 25 years in an industry that's not known to be particularly safe (drilling and mining), and I know what things were like in the old days, before management could care two whits about either safety or environmental protection.  We're all still paying for some of that attitude.  Miner's deaths used to be not worth mentioning, now they're major news and cautionary examples.  Needless to say, since OSHA and MSHA seeped into the culture of the industry (and it's still not completely there within some companies I wouldn't want to work for) deaths and injuries have gone way down, and environmental catastrophes have declined tremendously -- yet at the same time mining is more productive and efficient than ever before.  Those two facts are not unrelated.  The technology of mining has seen great innovation, in large part because of the requirement to protect human safety and the surrounding environment. 
Yes, mining is more expensive now, but the lives of miners are no longer as cheap, either.  It's more than worth the tradeoff.

This attitude can and should (and apparently does) apply to human spaceflight as well.  As stupendous and inspirational as Apollo was, it was extremely dangerous, and it was in large part a matter of luck that we didn't lose more astronauts and ground crew than we did.  Accidents like Challenger and Columbia are no longer acceptable, nor should they be.  We have to accept some risk, but we should always be pushing at the envelope of safety as well as capability.  Whatever you might like or not like about SLS, I think it's a step forward in that respect, and I'm hopeful that Space X is following that same path.  They have to, if the goal of making space accessible to all is ever to be achieved.

I'm 100% with you with respect to health, safety, environmental concerns, etc.  Ever notice how the same people that berate OSHA and the EPA are usually also the ones who berate China for not having any effective equivalents?

Apollo was indeed mad.  I often try to visualize, I mean REALLY visualize, the shear madness of piloting a practically-untested lunar lander, descending onto the actual eff-ing moon, and knowing that any one of 100 things will make you either crash or not be able to ascend.  It's mind-blowing.  There's no plan B, there's no undo or reset.  It's you, a joystick, and your surreal shadow down below.  Mad indeed.

They used to say "if people are not dying, we're not trying hard enough".

Today, however we are in absolute no danger of erring in that direction. What we have is a bunch of business and reputation risk-averse execs running everything.

When there's a malfunction, your typical present-day exec will immediately and without hesitation start working on severability of the chain of responsibility, so his ass is covered.  Civilian or military - people have been known to physically flee the site of a mishap in order to reduce association with it.

Risk no longer means "the chance having people killed".  It means "the chance of having our shares lower in value", or "the chance of having an association with a failed project on my resume".

See Jim's comment above about ULA "taking risk" by getting less than a 100% explicit guarantee from government that all their development costs  will be covered.
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Offline deltaV

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Re: First stage recovery at down-range locations
« Reply #38 on: 03/28/2013 12:52 am »
How much risk NASA and ULA do/should take is off-topic for this thread.

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Re: First stage recovery at down-range locations
« Reply #39 on: 03/28/2013 01:06 am »
The main issue with down range recovery, at least as far as SpaceX is concerned, is that it doesn't work for the "rapidly" part of Elon's often stated
 "Fully and rapidly reusable" mantra.

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