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SpaceX Successfully Launches Jason-3 Satellite, Rocket Landing Partial Success (theverge.com)

An anonymous reader writes: SpaceX successfully launched a Falcon 9 rocket today carrying the Jason-3 ocean monitoring satellite. "Jason-3 data will be used for monitoring global sea level rise, researching human impacts on oceans, aiding prediction of hurricane intensity, and operational marine navigation," NASA said. Unfortunately Space X reports that the attempt to land the Falcon 9 on a drone platform was only a partial success. According to the company twitter page: "First stage on target at droneship but looks like hard landing; broke landing leg." Update: 01/18 04:16 GMT by S : Here's a brief video of the landing attempt (somewhat loud).

118 comments

  1. It's really too soon for this post. by Rei · · Score: 2

    I didn't submit this news because really we barely know anything at the moment. Jason-3 is still awaiting its second burn, and without knowing anything more than "it has a broken leg" I think it's too soon to call the landing a "partial success". The second burn will be happening shortly, and they said we'd get more data about the landing in a few hours.

    Be patient, grasshopper.

    --
    He's the sort of person who would sell the Red Cross to Dracula.
    1. Re:It's really too soon for this post. by Rei · · Score: 1

      Jason-3 circularization burn underway.

      --
      He's the sort of person who would sell the Red Cross to Dracula.
    2. Re:It's really too soon for this post. by Dan+East · · Score: 4, Funny

      Wait a second. You're saying Slashdot is posting news too fast??? What alternate reality are we in?

      --
      Better known as 318230.
    3. Re:It's really too soon for this post. by Rei · · Score: 1

      Second burn completed successfully. Awaiting news of separation.

      --
      He's the sort of person who would sell the Red Cross to Dracula.
    4. Re:It's really too soon for this post. by Rei · · Score: 4, Informative

      Confirmation of Jason-3 separation. *Now* we can say that "SpaceX Sucessfully Launches Jason-3 Satellite".

      Now let's wait for news on the landing...

      --
      He's the sort of person who would sell the Red Cross to Dracula.
    5. Re:It's really too soon for this post. by mobby_6kl · · Score: 1

      Looks like second burn went well and payload was successfully deployed. Maybe the OP was just from the (very near) future?

      Calling the landing a "partial success" is probably a very optimistic way of putting it, as I imagine it likely hit the platform too hard (due to the waves?), broke one of the legs, and fell over, possibly with a big boom. Still, it's difficult to say without at least a video.

    6. Re:It's really too soon for this post. by Rei · · Score: 1

      Indeed, I have trouble picturing it being intact and upright after a (quote) "hard landing" and with a broken leg.

      --
      He's the sort of person who would sell the Red Cross to Dracula.
    7. Re:It's really too soon for this post. by rasmusbr · · Score: 4, Interesting

      The live stream froze just as a yellow reflection (rocket exhaust most likely) became visible on the surface of the ship, which probably means that the rocket was no more than 50 meters or so from the ship at that time. So it seems plausible that it hit the ship. I imagine SpaceX has recovered footage from the ship by now unless the antenna got hit by debris from the explosion.

      The fuel and the tank is quite fragile and at least one of the engines is extremely hot and located near the fuel tank, so unless the landing is perfect the tank will burst and the fuel will ignite. I expect we'll see some fiery footage within a day or two once they've had time to analyse it internally.

    8. Re:It's really too soon for this post. by Anonymous Coward · · Score: 0

      "Maybe the OP was just from the (very near) future?"

      Probably posting from Australia or New Zealand. They live in the very near future.

    9. Re:It's really too soon for this post. by Anonymous Coward · · Score: 0

      What alternate reality are we in?

      We are presently in the spacex fanboi reality distortion field, where boosters that tip over and blow up on landing are "partially successful."

    10. Re:It's really too soon for this post. by Ol+Olsoc · · Score: 1

      Looks like second burn went well and payload was successfully deployed. Maybe the OP was just from the (very near) future?

      Calling the landing a "partial success" is probably a very optimistic way of putting it, as I imagine it likely hit the platform too hard (due to the waves?), broke one of the legs, and fell over, possibly with a big boom. Still, it's difficult to say without at least a video.

      This is why I think that barge landing is pointless, unless it is on a nice still lake, or the barge is 100 percent stabilized. If teh barge is lifting, it can land too hard. If sinking it might be a little better. Just seems like an un-needed complication

      --
      The shepherds did so well protecting the flock that the sheep no longer believed that wolves existed.
    11. Re:It's really too soon for this post. by mobby_6kl · · Score: 4, Interesting

      This is why I think that barge landing is pointless, unless it is on a nice still lake, or the barge is 100 percent stabilized. If teh barge is lifting, it can land too hard. If sinking it might be a little better. Just seems like an un-needed complication

      Well they aren't doing it just for shits and giggles - landing on the barge requires significantly less fuel than returning all the way to the launch site. This, turn, reduces the payload capacity and increases the cost per kg.

      I do wonder how feasible it would be to build some sort of a hydraulically stabilized landing platform on top of the barge - not only could it compensate for the shitty weather, but also soften the landing if it detected the rocket coming in too fast.

    12. Re:It's really too soon for this post. by taiwanjohn · · Score: 2

      Unfortunately, they didn't make the landing. According to Elon via Twitter:

      Definitely harder to land on a ship. Similar to an aircraft carrier vs land: much smaller target area, that's also translating & rotating.

      Also:

      However, that was not what prevented it being good. Touchdown speed was ok, but a leg lockout didn't latch, so it tipped over after landing.

      It will be interesting to see how well they can zero-in on the 'carrier' landing in future flights. When you combine the trans-sonic approach with the chaos of ocean waves, the magnitude of this task is mind boggling. I can't wait. ;-)

      --
      XML is like violence. If it doesn't solve your problem, you're not using enough of it. --AC
    13. Re:It's really too soon for this post. by Rei · · Score: 1

      To be fair to the submitter, I think they just misinterpreted the news as meaning that the rocket didn't tip over and merely damaged a leg. That misinterpretation may be due to overoptimism on their part, but I'm not going to psychoanalyze them.

      --
      He's the sort of person who would sell the Red Cross to Dracula.
    14. Re:It's really too soon for this post. by laurencetux · · Score: 1

      so they do it a teched up version of how a carrier does it

      about 300 meters out they have they navcom on the platform tell the navcom on the stage to

      "Call the Ball"

      making sure the leg won't collapse would also be smart

    15. Re:It's really too soon for this post. by 93+Escort+Wagon · · Score: 1

      You know, it's just like how Apollo 1 was partially successful because no one in Mission Control got killed in the fire...

      --
      #DeleteChrome
    16. Re:It's really too soon for this post. by TheGavster · · Score: 4, Informative

      I also thought that going back to barge landings seemed like an unnecessary complication, as I was under the impression that the reason the first two attempts were at sea was because that proof-of-concept was needed to get permits for a ground landing. Today during the webcast, though, they clarified that for polar orbits such as this, they need to launch from Vandenburg in California, and there isn't a convenient piece of ground to land on.

      --
      "Because Science" is one step from "Because old book". Try "Because of my experiment testing my falsifiable assertion".
    17. Re:It's really too soon for this post. by DanielRavenNest · · Score: 4, Informative

      > I do wonder how feasible it would be to build some sort of a hydraulically stabilized landing platform on top of the barge

      Look up "Sea Launch", which was a partnership between Boeing, Kvaerner A.G. (Norwegian ship and drilling platform builder), and Russian rocket companies. They launched rockets from a converted drilling platform out in the Pacific Ocean.

      A semi-submersible platform like that takes on ballast water to lower the center of mass below the waves, while the platform on top is held *above* the water on columns. The waves can then pass through the columns without moving the platform much, because it's not a solid wall like the side of a ship. The ballast water mass also makes the whole platform more massive and hard to move.

      Right now (or very soon) you will likely be able to pick up drilling platforms for scrap value. With the price of oil so low, expensive ways to extract oil, like fracking and ocean drilling, can't make a profit, so the drilling companies stop doing it, and some of them go bankrupt.

    18. Re:It's really too soon for this post. by sysrammer · · Score: 1

      You know, it's just like how Apollo 1 was partially successful because no one in Mission Control got killed in the fire...

      No. Not like that. Not like that at all.

      --
      His ignorance covered the whole earth like a blanket, and there was hardly a hole in it anywhere. - Mark Twain
    19. Re:It's really too soon for this post. by catchblue22 · · Score: 4, Informative

      The latest tweets from Musk indicate that on reading the data, the landing was not "hard". Apparently one of the legs failed to lock. Also it landed 1.3m from the center.

      Elon Musk @elonmusk 6h6 hours ago

      Definitely harder to land on a ship. Similar to an aircraft carrier vs land: much smaller target area, that's also translating & rotating.

      Elon Musk @elonmusk 6h6 hours ago

      However, that was not what prevented it being good. Touchdown speed was ok, but a leg lockout didn't latch, so it tipped over after landing.

      Most of the posts in this discussion are based on incomplete information.

      --
      This and no other is the root from which a tyrant springs; when first he appears as a protector - Plato (423 to 327 BC)
    20. Re: It's really too soon for this post. by Anonymous Coward · · Score: 0

      This rocket was the last version 1.1 which does not have enough fuel to head back to the landing pad

    21. Re:It's really too soon for this post. by bored · · Score: 1

      Right, so why not pick somewhere that has land down range?

      I suspect that is part of the selection of south texas as a launch site. Launch it from texas, land it in florida.

    22. Re:It's really too soon for this post. by Michael+Woodhams · · Score: 1

      You can't sail a drilling platform up to a wharf to unload the rocket, like you can a barge (so your idea would require an extra transfer at sea from platform to barge), nor is it so easy to move around the landing spot to match mission requirements. Having said all that, if barge landings turn out to be sufficiently haphazard, your idea may be economical.

      --
      Quattuor res in hoc mundo sanctae sunt: libri, liberi, libertas et liberalitas.
    23. Re:It's really too soon for this post. by 12dec0de · · Score: 1

      Errm.. the type that DanielRavenNest was taking about (a semi-submersible) you CAN drive up to a dock. Its deck may be a bit higher than the "Just Read the Instructions", but thats what dock side cranes are for.

    24. Re:It's really too soon for this post. by Michael+Woodhams · · Score: 1

      Thanks, that's great.

      I wonder why SpaceX didn't start with this design?

      --
      Quattuor res in hoc mundo sanctae sunt: libri, liberi, libertas et liberalitas.
    25. Re:It's really too soon for this post. by Rei · · Score: 2

      Generally, having land downrange is considered a bug, not a feature. It makes permitting very hard because nobody likes the concept of half a million kilograms of explosive fuel and oxidizer along with tons of shrapnel-aluminum skin and big heavy engines landing in their town in the event of failure where the self-destruct mechanism doesn't do its job.

      That said, yes, Florida is probably enough downrange so as not to be a major source of concern. Still, I'd think it would be too far for Falcon 9 boosters, at least on most missions. Maybe it would be suitable for Falcon Heavy's core stage, though.

      --
      He's the sort of person who would sell the Red Cross to Dracula.
    26. Re:It's really too soon for this post. by lars_stefan_axelsson · · Score: 1

      Cost. Drilling or production rigs are a couple of magnitudes more expensive than the barge they use now. As it seems to be, almost sort of, working, there's no need to spend that much extra. They're trying to be the cheaper alternative to the likes of the ULA, remember? ;-) (You can always buy a bigger one later, but if you start with too big, then that's sunk cost).

      (The ULA OTOH would probably have bought two brand new off shore platforms, ice rated ones, and gold plated them. Just because... ;-))

      --
      Stefan Axelsson
    27. Re:It's really too soon for this post. by david_thornley · · Score: 1

      It seems to have hit the target, and since Space-X is trying to do something really new I'm happy calling that a "partial success". Complete failure would have just dropped the stage into the briny. In the meantime, the primary mission was a complete success.

      --
      "When you have eliminated the unacceptable, whatever is left, however improbable, must be the truthiness" - Holmes
    28. Re:It's really too soon for this post. by Anonymous Coward · · Score: 0

      Fuck You.

      Grissom, Chaffee, and White were my childhood heroes.

      And still are.

    29. Re:It's really too soon for this post. by Anonymous Coward · · Score: 0

      Yeah.

      https://www.youtube.com/watch?v=OVU5fsVfuNs

  2. if there's anything I learned playing KSP by Anonymous Coward · · Score: 0

    it needs more struts

    1. Re:if there's anything I learned playing KSP by AC-x · · Score: 1

      It fell over, so clearly the problem is not enough RCS thrusters!

  3. Jason-3 deployed successfully by Anonymous Coward · · Score: 0

    Jason-3 deployed successfully - Rocket broke leg on landing and exploded.

    1. Re:Jason-3 deployed successfully by Rei · · Score: 1

      No confirmation yet on explosion, though that sounds probable.

      --
      He's the sort of person who would sell the Red Cross to Dracula.
    2. Re:Jason-3 deployed successfully by Anonymous Coward · · Score: 0

      Well, I *saw* it explode. Go back to the teacher's lounge.

    3. Re:Jason-3 deployed successfully by Rei · · Score: 1

      Please learn the meaning of the word "yet". There was no video of the event at the time, nor anyone on the barge who could have seen it.

      You can learn new words in the teacher's lounge.

      --
      He's the sort of person who would sell the Red Cross to Dracula.
  4. sea-legs by N3wsByt3 · · Score: 1

    The rocket clearly has no sea-legs. ;-)

    It's curious though, that the only really successful landing was on land. I always thought it was because it is so much more difficult, getting to land on a small surface, bouncing on the waves, but when I read the actual papers on it on the site of SpaceX itself, it seemed it never had anything to do with it. It were things like: to few fuel, or a computer-glitch that caused a delay in steering, etc.

    Yet...once again, it goes wrong on the drone/barge. Are they just extremely unlikely, or IS it actually so much more difficult to do on there, even when they don't give any indication of it themselves?

    --
    --- "To pee or not to pee, that is the question." ---
    1. Re:sea-legs by Anonymous Coward · · Score: 0

      I always wondered why they don't put like springs or shock absorbers, etc. on the "legs" to somewhat compensate for the movement of the landing surface.

    2. Re: sea-legs by Anonymous Coward · · Score: 0

      yeah too bad the barge cant have some sort of isolating gymbal that keeps the pitching of the barge independent from landing surface.

    3. Re:sea-legs by Rei · · Score: 1

      Even if we assume a perfectly stable platform, the fact that the drone ships are so much smaller than the ground landing pad means that the rocket has to do much more precise corrections to ensure that they land on it.

      We'll find out soon enough what happened here.

      --
      He's the sort of person who would sell the Red Cross to Dracula.
    4. Re:sea-legs by rasmusbr · · Score: 1

      The previous times that they have attempted to land on a drone ship have all failed due to failures that happened earlier in the descent, so they haven't been able to test how the touchdown itself will work at sea, at least not before today.

    5. Re:sea-legs by Anonymous Coward · · Score: 1

      But we've seen that after the first two landing attempts it has no problem landing on a dime. The barge moving up and down however is a little trickier to predict.

    6. Re:sea-legs by NEDHead · · Score: 1

      Smaller perhaps, but if you watch the on-land successful return, they hit the bullseye, so I doubt the size is the issue.

      Pitching & rolling, and a varying vertical location seem to be harder problems, plus they rocket was an earlier version that may have been less capable than the previous flight.

    7. Re:sea-legs by Rei · · Score: 2

      It did hit the bullseye, but it didn't have to.

      Regardless, we now know that this incident was due to "Touchdown speed was ok, but a leg lockout didn't latch, so it tipped over after landing." The question is why the leg didn't latch.

      --
      He's the sort of person who would sell the Red Cross to Dracula.
    8. Re:sea-legs by Anonymous Coward · · Score: 0

      landing an airplane on an aircraft carrier in daylight and sea state 0 during the day is not trivial, either.But we still do it, routinely. even with dorky C2 & E2's. we've even done it with C130s too.
      it took more than a few crashes and "bolters" to get that process to where it is today, too.
      at least with helicopters they can tether them and winch them down to the deck in shitty weather and sea conditions far worse than they normally would.
      helicopters can hover, the Falcon can't.
      it's gotta be a non trivial control systems programming excercise, with the moving platform adding a couple degrees of difficulty to it.

    9. Re:sea-legs by nick1austin · · Score: 1

      They did. When the engine turns off you see the Falcon drop slightly and the legs splay out a little.

  5. Ground Control To Major Tom by Anonymous Coward · · Score: 0

    Musk baby doesn't want the investors to see the fireball than consumed the Falcon 9 and sunk the "Just Read The Instructions" lander.

    OOOOOOPPPPPPPPSSSSSSSSS!!!!!!

    Ha ha

  6. Space X by Anonymous Coward · · Score: 0

    Space X or someone needs to move to Burns Flat Oklahoma.

  7. Why is the ship a "drone"? by Anonymous Coward · · Score: 0

    Or are we just fellating Musk some more?

    1. Re:Why is the ship a "drone"? by Rei · · Score: 4, Informative

      Because it has no crew and is remote controlled, with various automated features such as locking to specified GPS coordinates..

      I'm not sure why you're confused about this.

      --
      He's the sort of person who would sell the Red Cross to Dracula.
    2. Re:Why is the ship a "drone"? by Anonymous Coward · · Score: 0

      I'd like to believe that the GP was being sarcastic. We see the word "drone" being used for everything nowadays, so perhaps he was being sarcastic, with this particular usage being one of the few good ones?

  8. "Update" (not really) by Rei · · Score: 1

    New tweet from Musk, but no new news:

    Definitely harder to land on a ship. Similar to an aircraft carrier vs land: much smaller target area, that's also translating & rotating.

    --
    He's the sort of person who would sell the Red Cross to Dracula.
  9. Actual update! by Rei · · Score: 4, Informative

    Oooh, actual news:

    However, that was not what prevented it being good. Touchdown speed was ok, but a leg lockout didn't latch, so it tipped over after landing.

    Great to have the update. Not so great for whatever people were in charge with making, prepping, and inspecting the legs ;) Unless it was a design flaw.

    I guess we have a new question now - why it didn't lock.

    --
    He's the sort of person who would sell the Red Cross to Dracula.
    1. Re:Actual update! by Brandano · · Score: 1

      What I wonder is, since it is already landing on a relatively small spot, why can't they set up the ship to catch it and prevent it from toppling over? A system of cables like the one used for catching the Ryan X-13 Vertijet should not be impossible.

    2. Re:Actual update! by ColdWetDog · · Score: 4, Insightful

      The booster is strong in only one direction - the longitudinal one. If you try to catch it with cables, it goes on it's sides which are just thin walled aluminum, Like a giant beer can. It's a matter of weight. Tradeoffs.

      --
      Faster! Faster! Faster would be better!
    3. Re:Actual update! by Brandano · · Score: 1

      True, but I think that having a dented tank to replace might come out cheaper than having to fix an entire first stage that has toppled over

    4. Re:Actual update! by Anonymous Coward · · Score: 0

      The actuator and locking servo were negatively affected by the gravitational pull of Donald Trump's toupee.

    5. Re:Actual update! by Anonymous Coward · · Score: 0

      Isn't the real cost in the engines?

      If the whole assembly falls over and explodes, you loose these.

      If the assembly is caught by a cable, you dent the body, but you save the engines.

      ??

    6. Re: Actual update! by Anonymous Coward · · Score: 0

      Why not land into a giant spider web??!!

    7. Re: Actual update! by sysrammer · · Score: 1

      Why not land into a giant spider web??!!

      ...or a Cat's Cradle...

      --
      His ignorance covered the whole earth like a blanket, and there was hardly a hole in it anywhere. - Mark Twain
    8. Re:Actual update! by catchblue22 · · Score: 1

      This was the last launch of v1.1 of the Falcon 9. As I understand it, v1.2 (sometimes called v1.1 Full Thrust) has upgraded landing legs. In either case, I would not call this a failure. The payload was placed into orbit. The touchdown speed was in fact normal. For some reason, one landing leg didn't lock. The landing is considered an experiment anyways. Isn't it good to do experiments? Don't you learn from them?

      --
      This and no other is the root from which a tyrant springs; when first he appears as a protector - Plato (423 to 327 BC)
    9. Re:Actual update! by Anonymous Coward · · Score: 0

      Yeah, they should come up with some ropes that are attached to three of four towers on the corner of the barge. Then when the rocket is close to touching down, the center tower releases it's rope and they get pulled tight.

      Even if it is just a backup, it wouldn't take much to implement.

    10. Re: Actual update! by Anonymous Coward · · Score: 0

      Unicorn fur.

  10. Latest update: by Rei · · Score: 1

    After further data review, stage landed softly but leg 3 didn't lockout. Was within 1.3 meters of droneship center

    úff....

    --
    He's the sort of person who would sell the Red Cross to Dracula.
    1. Re:Latest update: by Rei · · Score: 4, Informative

      Well, at least the pieces were bigger this time! Won't be last RUD, but am optimistic about upcoming ship landing.

      Musk provides the first pic. Actually, I expected worse. They can probably scrap this one for parts and send them off to destructive testing.

      --
      He's the sort of person who would sell the Red Cross to Dracula.
  11. Maybe bezos should show him how by stabiesoft · · Score: 1

    He gets to claim the first to land one on soil, maybe he could try it on water and get bragging rights to water too. Billionaire problems.

  12. 4 legs look not very stable. Why not 6 - 8 legs? by laserhead · · Score: 1

    4 legs look not very stable. If one leg failed, the rocket would fall. Why not 6 - 8 legs?

  13. Enthusiasm for today's launch at Vandenberg by Whatsmynickname · · Score: 1

    Was on Ocean Avenue this morning for today's launch, and although you didn't see the rocket go up this time (too foggy), the thing that made me the happiest was all the 20 year old people out there today (a lot from SpaceX as from their jackets) watching the event also. Ton's more people out there today than an average launch there! I am so glad at least there is a new generation of people who are genuinely interested in space, the development of new space technology, and working for a place which they are interested in. This is so refreshing from the aerospace I've known before...

  14. Does it have to be the whole booster? by N3wsByt3 · · Score: 1

    I note some are saying it makes sense to let return the whole booster/first stage, and that the center of gravity is at the bottom anyway, so it makes sense to go for the whole packet.. but I dispute that.

    Purely speaking from an economic standpoint, it would also make sense to do things differently.
    One could also just go for the most expensive part, which are the engines and avionics, and, depending on how you manage to retrieve them, it could actually be better. This isn't really all that far-fetched. Arianespace (EU) is thinking exactly that, for a further development of the Ariane 6, after it gets build. It's partially reusable, and it's called Adeline.

    See https://en.wikipedia.org/wiki/... for more info.

    And since it only would use 2000 kg versus 35000kg with SpaceX (and thus, also effects the usable payload one can get in orbit), there is actually a commercial case to be made for it.

    --
    --- "To pee or not to pee, that is the question." ---
    1. Re:Does it have to be the whole booster? by Anonymous Coward · · Score: 0

      Well, that's what we call competition, different companies have different ideas and try different things.

      We will see how things work out. It may be easier to throw away most of the first stage and just collect the 'expensive bits', but it takes a lot more work to re-use those expensive bits if you have to build a new first stage.

      Space-X is aiming for a much faster turnaround than you could get from building an entire first stage every time.

      I don't know where you are getting your 2K kg vs 35K kg, is that the weight of the expensive bits vs the weight of the entire first stage? or are you claiming that the weight cost to recover the expensive bits vs the entire first stage is that large?

    2. Re:Does it have to be the whole booster? by AHuxley · · Score: 1

      Re 'Purely speaking from an economic standpoint, it would also make sense to do things differently."
      Have a look at the other ideas. Cheaper, more smart to get the mission done, much less complex and they could offer more up in space with what could be moved up from earth.
      The US has always had a fixation with a bring back down option. Why would the US demand a soft, safe land return?

      A few ideas about burn up or public ocean return got offered and got rejected.
      In the back of the US military industrial complex is one long term design option the US wants passed onto its design team.
      The need to collect a nations space equipment and return it to any selected US military base when needed.
      Allowing a long term team to win with burn up or an public ocean recovery would set a bad technological design trend that would stop providing public and science design cover stories for dual use military ready missions.

      Long term its back to a dual use Space Shuttle landing like landing system with big cargo room to sell the wider public on cute science while offering the military large cargo up and down options.
      "Declassified US Spy Satellites Reveal Rare Look at Secret Cold War Space Program" (September 20, 2011)
      https://news.yahoo.com/declass...
      "The space shuttle's payload bay was sized to accommodate the KH-9".

      --
      Domestic spying is now "Benign Information Gathering"
    3. Re:Does it have to be the whole booster? by Rei · · Score: 1

      Which is why we do that with airplanes, right? ;)

      --
      He's the sort of person who would sell the Red Cross to Dracula.
    4. Re:Does it have to be the whole booster? by N3wsByt3 · · Score: 1

      Well, it's explained in the wikipedia (link) I posted, no?

      It refers to the weight of fuel being spend to return safely to Earth. The best estimates of SpaceX' approach to land the whole first stage by using it's engine, is around 35-40 K kg. In contrast, Adeline uses a winged return, and then some small deployable propellers, and would only use 2000 kg of fuel.

      This also makes a fairly huge difference in maximum usable payload, where SpaceX loses between 30 and 50% that way, Adeline would lose less than 10%.

      --
      --- "To pee or not to pee, that is the question." ---
    5. Re:Does it have to be the whole booster? by catchblue22 · · Score: 1

      Purely speaking from an economic standpoint, it would also make sense to do things differently. One could also just go for the most expensive part, which are the engines and avionics, and, depending on how you manage to retrieve them, it could actually be better.

      Yeah, I hear the engines and avionics are the most expensive part of a 747. Who don't we just ditch the fuselage after every flight, and keep the engines and avionics. Would that make economic sense?

      You sound like a ULA shill.

      --
      This and no other is the root from which a tyrant springs; when first he appears as a protector - Plato (423 to 327 BC)
    6. Re:Does it have to be the whole booster? by tsotha · · Score: 1

      They had to "while [offer] the military large cargo up and down options" because the only way they could make the numbers sort of work when they sold it to Congress was to assume the shuttle would do all US launches. It was a raid on the Air Force's space and missile systems budget. The Air Force was livid, too, since it was obvious NASA would never be able to deliver.

    7. Re:Does it have to be the whole booster? by N3wsByt3 · · Score: 1

      That would be an Arianspace-shill, if I were a shill, since Adeline is of the EU space-program (by airbus). ;-)

      I'm not certain why you're being so defensive. I merely pointed out that, if you compare the projects of having the whole first stage come back, and an Adeline-esque approach, the latter seems to have an economic advantage.

      It doesn't mean I'm not a proponent of re-usability, but if you're going to invoke that sort of analogy, you'd have to compare it to something like Skylon, with its sabre-engines. As far as it goes now, your analogy is a bit lacking. To make it correct, one would need to change the following: only about half of the 747 is being recuperated anyhow (thus, still making it very expensive). And of that half, about 80% of the costs can be recuperated by just returning the engines and avionics. To recuperate that last 20% of half of the 747 (aka, 10% of the total cost), you'll use up and lose 30 to 50% of your cargo/passenger potential.

      Seen, like that, then: yes, it certainly could make economic sense to go for an Adeline approach. It merely depends on a cost-benefit analysis.

      --
      --- "To pee or not to pee, that is the question." ---
    8. Re:Does it have to be the whole booster? by stevelinton · · Score: 1

      The key element is cost/speed of turnround. The fuel tanks in a first stage may not be very expensive, but hooking up and testing new tanks will take time, and then checking the integration takes more time. SpaceX are aiming for a model where there is not much more to do that pump in fuel, a cursory visual inspection and ask the avionics to self-check. Engines would need a full inspection every so many firings. If they can pull this off it almost has to be cheaper than any model involving more reintegration.

    9. Re:Does it have to be the whole booster? by N3wsByt3 · · Score: 1

      See my response to catchblue22.

      Do note it's a comparison between SpaxeX' first stage return and something like Adeline. Nothing more, nothing less. If airplanes would have the same cost-benefit considerations as rockets, then yes, we would do that with planes too.

      --
      --- "To pee or not to pee, that is the question." ---
    10. Re:Does it have to be the whole booster? by Rei · · Score: 1

      The whole point of what SpaceX is doing is to make the economics like those of airplanes. They want airplane-like economics. Arianespace is seeking economics that would never work out with airplanes.

      And yes, the engines and electronic systems on an airplane are way more expensive than the fuselage.

      --
      He's the sort of person who would sell the Red Cross to Dracula.
    11. Re:Does it have to be the whole booster? by TechnoCore · · Score: 1

      Ask yourself if throwing away everyting but the engines from a Boeing 787 after each landing would make your airplane ticket cheap or not.
      There would be no air planes at all on this earth if that solution was used for air travel.
      Space-X is aiming for rapid reuse to drive costs down to a fraction of what they are today. Just saving the engines is not a solution if you have that goal.

    12. Re:Does it have to be the whole booster? by N3wsByt3 · · Score: 1

      Yes, but that was not the contention I made. AS LONG AS the economics are not similar to that of airplanes - and frankly, without systems similar to Skylon, where you actually use the air in the atmosphere, you'll never get there - the question remains what is the most economical. And if you compare the first stage of spaceX with something like Adeline - which was what I compared - then you can definitely make an economic (better) case for the latter.

      One can argue it's only a short-term or mid-long term better economic solution, but that doesn't change the fact that it IS economical more fruitful as of yet, and it will remain so, until you have a completely different system which is, actually, comparable with airplanes.

      --
      --- "To pee or not to pee, that is the question." ---
    13. Re:Does it have to be the whole booster? by N3wsByt3 · · Score: 1

      See my answer to a similar remark here: http://slashdot.org/comments.p...

      --
      --- "To pee or not to pee, that is the question." ---
    14. Re:Does it have to be the whole booster? by N3wsByt3 · · Score: 1

      It wouldn't take more time than for any other module or stage to be connected, which is always the case, with rockets who have 2-3 stages (which are the vast majority of rockets).

      The extra time and efort needed, compared to everything else, would be minimal. It's hardly a strong rebuttal, just like saying "it will take spaceX more time to check the tanks out too". As long as you can keep refurbishing costs low, the testing and hooking up are trivial costs compared to all the rest.

      --
      --- "To pee or not to pee, that is the question." ---
    15. Re:Does it have to be the whole booster? by Rei · · Score: 1

      Yes, but that was not the contention I made. AS LONG AS the economics are not similar to that of airplanes

      Which, according to the contention that I just made, if SpaceX is right then they will be like airplanes in the near-to-mid term. Pointing out that they're not like airplanes at this exact second is meaningless.

      and frankly, without systems similar to Skylon, where you actually use the air in the atmosphere, you'll never get there

      Nonsense. Propellant is cheap. The propellant cost to orbit is a couple dozen dollars per kilogram - 0,1% to 1% the cost of the launch. You don't need airbreathing engines. You need to not throw away your $70+m rocket after every flight. And, for that matter, not spend tens of millions of dollars spread out between making new tanks, reintegrating your recovered electronics and engines, extensively retesting the whole assembly (since it's basically a new untested rocket), retransporting it from the factory to the launch site, and all of the other pieces of overhead that make up much of that ~$70m+ cost to begin with.

      And if you compare the first stage of spaceX with something like Adeline - which was what I compared - then you can definitely make an economic (better) case for the latter.

      You can certainly try, but you've hardly even attempted that thusfar, just repeatedly asserting that returning the engines and avionics is somehow cheaper than getting a whole intact rocket back at the launch pad or on a barge ready to be hoisted back onto the launch pad.

      but that doesn't change the fact that it IS economical more fruitful as of yet

      Writing the word IS in capital letters doesn't change anything written above.

      --
      He's the sort of person who would sell the Red Cross to Dracula.
    16. Re:Does it have to be the whole booster? by Enigma2175 · · Score: 1

      And if you compare the first stage of spaceX with something like Adeline - which was what I compared - then you can definitely make an economic (better) case for the latter.

      Yes, but you're comparing something that is currently flying to something that has absolutely no flight hardware developed. Adeline is just a dream in some CAD designer's mind at this point. Once they actually develop something (they are saying 2025 for first flight, so count on 2030 or later) then you can make comparisons but until then there is nothing to compare.

      --

      Enigma

    17. Re:Does it have to be the whole booster? by stevelinton · · Score: 1

      Fair enough. You're effectively increasing the stage count by 1 (although the extra stage has no engines) so you'll need to pay the mass for the connectors between the engine stage and the fuel tank stage, and the structural elements needed to make the two stages independently handleable.

      I guess the next few years will tell us which approach best suits todays materials, engines, fuels and building techniques. Should be interesting.

    18. Re:Does it have to be the whole booster? by N3wsByt3 · · Score: 1

      No, but using capital letters stresses the importance of what you want to convey.

      Anyway, you're missing the point.

      The point was and is NOT (stressing this) that SpaceX might or might not make rocketry 'like airplanes' in the mid- or longterm (which, after all, even you can't know for sure they'll succeed), but that the current system of having the FIRST STAGE (stressing this again) of a rocket coming back by using their fuel, compared to a system like adeline, is less economical advantageous.

      I'm not sure why you keep negating that. It's just elementary cost-benefit analysis.

      Now, YOU can make the contention that SpaceX will make it like airplanes, but that does NOTHING to change the fact that, as long as it doesn't, adeline is economically more beneficial. So the comparison was between the system of SpaceX first stage, and Adeline. Not between Adeline and an unknown future where rockets may or may not be 'like airplanes'. So me pointing this out is not 'meaningless', since it's a comparison not a comparison bewteen adeline and some future where SpaceX manages to reduce the total cost similar to that of airplanes, between those two systems of having a partially recovery of the rocket, nothing more, nothing less.

      I hope I made this clear.

      Now, as for your further argumentation... may I ask, if you even read the page to which I linked? Because it doesn't seem you bothered. Otherwise, you would already know that the major 'cost' is NOT (stressing this again) the fuel, but the fact that the added weight reduces the capacity of usable payload. I assume you realise that to propel 1 pound of mass would require 9.39 pounds of propellant? This means, that if you need 35000 kg extra to land the thing, you'll need 9 TIMES as much to get it up. That's why, if you didn't realise this, that SpaceX never lands the first stage when it has to deliver a heavy geostationary satellite in orbit: it's because they need all the fuel to get their payload up there. Ergo, the fuel they spend on it, needs more fuel to lift it, and that inveriably reduces the amount of weight of the payload they can send up. There is no way around this.

      And that is only for the first stage. The second stage - and if they want to be 'like airplanes', you'll need to recuperate all stages - is going to be much, much more difficult to recuperate. But worse, this, in turn, will need, again, extra fuel, to transport the fuel tht will be needed to land it. WORSE STILL: since now the second stage is much heavier, that weight will need to be lifted by the first stage too, so that will need even MORE fuel, which in turn will need 9 times more fuel to lift this up too. Then we come to the third stage. Rince, repeat. It needs extra fuel to land, thus it gains weight, thus the second stage needs ectra fuel, plus it needs extra fuel to lift that extra fuel, plus the third stage who has to lift all the other stages up needs extra fuel to do so, and it needs extra fuel to lift that extra fuel.

      Ergo: it gets exponentially more difficult to launch a rocket where all stages are recuperated. Or let me refrase that: it becomes exponentially more difficult for it to be economically viable, compared to a system where you'll only need a fraction of the mass to put the same payload into orbit.

      Thus, as I said, there is definitely an economic point to be made to use other systems, like that of Adeline.

      Note that this is an inherent problem, not just a mere technical problem. You'll ALWAYS have an exponentially increasing weight ratio for ever kg that is added as fuel or payload. The only way to starkly reduce the weight, at least of the first stage, is a system like Skylon, where you use the atmosphere, instead of carrying all your oxygen with you.

      "You can certainly try, but you've hardly even attempted that thusfar, just repeatedly asserting that returning the engines and avionics is somehow cheaper than getting a whole intact rocket back at the launch pad or on a barge ready to be hoisted back onto the launch pad."

      --
      --- "To pee or not to pee, that is the question." ---
    19. Re:Does it have to be the whole booster? by N3wsByt3 · · Score: 1

      Partially true. But I'm sure Arianespace had quite some people calculating it, so it's not like it sucked out of their thumb or comes out of the blue.

      It's like some here compare rocketry 'like airplanes' with that of Adeline: that's just a dream too.

      My only point was, that there could be made a good case for other systems, like adeline, that were economically more beneficial. As far as one can read the arguments (http://www.space.com/29620-airbus-adeline-reusable-rocket-space-tug.html), that seems to me to be the case.

      Frankly, saying it hasn't proven anything... well, spaceX hasn't proven they could reuse the stage neither, nor proven they are 40% cheaper than ordinary use-once rockets. Thusfar.

      Which doesn't mean I don't believe they don't have a good chance of doing exactly what they say, but as far as having actually demonstrated a beneficial economic advantage, they didn't prove anything neither, and it's still 'a dream' too. Just saying one can't use an argument without applying reciprocity.

      I think some posters here react a bit too ideologically. I mean, I'm all for Musk and SpaceX too, and I applaud thee efforts. but that doesn't mean we shouldn't look at things objectively. It's quite possible that systems like adeline, for the first stage, compared to a total 1st stage retrieval, could be more cost-effective, and thus, more economically viable. I say there can be made a good case for that, nothing less, nothing more.

      --
      --- "To pee or not to pee, that is the question." ---
    20. Re:Does it have to be the whole booster? by N3wsByt3 · · Score: 1

      My thoughts exactly.

      A lot of people react like being stung by a wasp by my post.

      It's like I said I despised Elon Musk and SpaceX or something, while I'm a fervent supporter of him/it, in fact. I think they have done great things.

      I'm just saying there can be made a good, and perhaps even better, (economical) case for other systems like that of Adeline, compared to the whole-1st-stage retrieval. The main problem being the extra fuel. No so much because of the cost of the fuel, as some misinterpret and don't grasp here on slashdot, but because of the *weight* of that fuel, which directly cuts into the usable payload for a given rocket.

      But as you said: the more diverse methods and techniques being tried out, the better.

      --
      --- "To pee or not to pee, that is the question." ---
    21. Re:Does it have to be the whole booster? by rpstrong · · Score: 1

      Yes, but you're comparing something that is currently flying to something that has absolutely no flight hardware developed. Adeline is just a dream in some CAD designer's mind at this point. Once they actually develop something (they are saying 2025 for first flight, so count on 2030 or later) then you can make comparisons but until then there is nothing to compare.

      To be fair, they do have a scale model flying. [I wonder where SpaceX will be in ten years, considering that they went from zero to earth landing in under 14 years.]

    22. Re:Does it have to be the whole booster? by N3wsByt3 · · Score: 1

      Indeed.

      Well, anyhow, I don't know why some people react like being stung by a bee for pointing out there could be better (in the economical sense) ways of doing things than the current system SpaceX used. Is this fanboism? I mean, *I* am a fan of Musk and spaceX too, but not to the point of being blind to other things.

      It is as you say: who knows where SpaceX will be next decade. The major issue now, is the way they recuperate it (by using their engines and thus burning loads of fuel). It's quite possible they'll develop a winged variant in the future, which doesn't have those disadvantages anymore. In the long term, I think Musk is right in wanting to recuperate everything, if you ever want it to become 'like airplanes'. That said, ultimately, I think systems like Skylon will take the spotlight, though.

      --
      --- "To pee or not to pee, that is the question." ---
  15. Re:4 legs look not very stable. Why not 6 - 8 legs by Spy+Handler · · Score: 1

    more legs = more weight and more motors and things to go wrong.

    Jet aircraft only have 3 legs even though if any one of them fails to open, it's in serious trouble. Why not 8 legs? Weight, man.

    Aircraft builders have solved this problem by making the 3 legs very reliable. They very rarely fail to open. SpaceX just needs better legs.

  16. 3 in the green by argee · · Score: 1

    One of the first things a pilot learns when coming in to land, is to have "3 in the green",
    which are the indicator lights for each of the landing gear legs to be down and
    locked. If not, you abort the landing.

    In this case, abort was not an option ...

  17. Platform questions by Anonymous Coward · · Score: 0

    If the booster was just sitting on the platform and the sea state was what they are seeing, would the rocket be able to just sit there?
        (Cg margins ok? forces on the structures ok? Slosh in the tanks ok? No tiedowns?)

    How nimble is the servo loop used to actually set down?
    How fast can the barge move in a new direction?
    How fast can the servo respond?

    Do the legs have any compliance, or are they fixed?
    If they are fixed, is one bigger than the rest, so you can touch on it first and then touch more legs?

    I still think the boat needs a 6dof capture device to reach out and grab the rocket and smoothly transition to forcefully holding it.

    Great job getting this far though.

  18. Re:4 legs look not very stable. Why not 6 - 8 legs by mobby_6kl · · Score: 3, Funny

    You need better legs and not more legs, that's what I kept telling my ex-girlfriend, too. That didn't work out too well, though maybe Elon will have more luck.

  19. Here's the video of the landing.Damn it was close by Anonymous Coward · · Score: 2, Informative

    Here's the video of the landing :https://www.instagram.com/p/BAqirNbwEc0/

    The rocket made a near perfect landing, even better than the last one. It must be so frustrating for SpaceX team to fail because of something like this.

  20. Safety for civilians on the ground by Max_W · · Score: 0

    In the last discussion someone wrote that there is almost no fuel inside while it is landing. I see that there is a lot of fuel to explode even after landing.

    If it deviates from a course while landing (what a hundred or two of kilometers for such a vehicle) and falls on a densely populated are, the damage may be significant. A parachute landing of an empty parts looks safer to me.

    1. Re:Safety for civilians on the ground by Rei · · Score: 1

      The Shuttle SRBs were parachute landings. They landed at nearly highway speeds. It's hard to parachute land a gigantic, fragile object and have it be intact. And seriously, parachutes are way more likely to go offtrack than engine-guided landings.

      --
      He's the sort of person who would sell the Red Cross to Dracula.
    2. Re:Safety for civilians on the ground by Max_W · · Score: 1

      Smart parachute technology is developing too.

      The problem with a rocket fuel explosion is that its detonation could burn out oxygen in an area, and there could be as a result unpredictable pressure fluctuations, which could hurt humans. Let alone the risk of starting a fire. Obviously, for a landing they keep quite an amount of fuel in reserve. It is impossible to land an aircraft with zero fuel exactly.

      In my opinion, it is safer to burn all the fuel high in the air and use the abundant clean energy of gravity for landing.

    3. Re:Safety for civilians on the ground by Rei · · Score: 1

      Slow means big parachutes.
      Big parachutes means heavy.
      Heavy on a first stage means "no payload fraction to orbit".

      A rocket explosion will not "burn out oxygen in an area"; rockets have their own oxidizer, in roughly stoichometric ratios with their fuel.

      You cannot burn 100% of your propellant, the tanks do not completely drain.

      --
      He's the sort of person who would sell the Red Cross to Dracula.
    4. Re:Safety for civilians on the ground by Anonymous Coward · · Score: 0

      The stages "explode" when they fall over because their fuel tanks are pressurized (with helium I believe), when the tanks are breached they pop like balloons at which point the little fuel that is left in them aerosolizes, when the aerosolized fuel hits the still extremely hot engine bell it ignites just as surely as if it had hit a spark plug. I imagine one of the first things that the stage does after it has successfully touched down is to bleed off most if not all of the pressure in the tanks.

    5. Re:Safety for civilians on the ground by rpstrong · · Score: 1

      It is impossible to land an aircraft with zero fuel exactly.

      Sadly enough, pilots continue to do so - with all-too-often fatal results.

  21. Re:4 legs look not very stable. Why not 6 - 8 legs by tsotha · · Score: 1

    Did she explode too?

  22. to Land or not to Land, is a secondary question! by 12dec0de · · Score: 1

    I want to congratulate E.M. on the near thing. I see a lot of discussion on whether ./ is full of fanboys or whether the legs are shite.

    You are all missing the main point of success: do any of you remember seeing such a rate of launches? Ever?

    Who cares if a few of them tip over. Just get better on the next try.

  23. Re: Here's the video of the landing.Damn it was cl by Anonymous Coward · · Score: 0

    Frustrating, but also not - a leg-lock collet freeze is just dumb engineering. It's clear where the fault lies, the legs are removable for upgrading -- sure, we got a kaboom, but an iterative improvement is easy and quick to apply.

  24. Classic technology by Max_W · · Score: 1

    It seems there is no better technology to fly to the Space as the one developed at Baikonur in 1957 https://en.wikipedia.org/wiki/... . Get over it, and just keep copying what the Great Engineers and Scientists built. It was not patented.

    1. Re:Classic technology by Pseudonymous+Powers · · Score: 1

      It seems there is no better technology to fly to the Space as the one developed at Baikonur in 1957 https://en.wikipedia.org/wiki/... . Get over it, and just keep copying what the Great Engineers and Scientists built. It was not patented.

      There is certainly much to be proud of in the old Soviet space program, but I'm not sure any of that is contained in the article you linked to, which seems to be about the Baikonur Cosmodrome itself. Most of the article is a history of how they decided where to put it, and a list of the exact coordinates of a bunch of individual launch pads. There's not a lot of technology mentioned in that article, unless you consider latitude and longitude a technology.

      If you're suggesting that a modern space program should exclusively use 1950's technology, well, where would we even find that many vacuum tubes and that much asbestos?

    2. Re:Classic technology by Anonymous Coward · · Score: 0

      Not quite sure what you're getting at, the satellite was successfully put into orbit. I don't believe that the Russians ever tried to recover the first stage of an orbital launch vehicle. And this is exactly the kind of rocket development program that the Russians believed in, quickly build and launch piece after piece of hardware and see if it works, if it doesn't make a few quick tweaks and try again. This is of course different from the NASA methodology of trying to design everything on paper and then building the final vehicle and expecting it to work right on the first launch.

    3. Re:Classic technology by Max_W · · Score: 1

      ... the old Soviet space program, but I'm not sure any of that is contained in the article you linked to, which seems to be about the Baikonur Cosmodrome itself. ... a modern space program should exclusively use 1950's technology...?

      Baikonur was an international effort, people of many nationalities worked there. I was a student of a mathematician who participated in the calculation of the first Earth's artificial satellite orbit in 1957. And I saw on TV the SpaceX's team chanting: "USA, USA,...", after a partial success last time.

      Trust me, these people will never do any innovation even remotely in the league of what was done in 50s at Baikonur. Those engineers and scientists, who really did it in 50s, worked for humanity, for science, and for SpaceX employees it seems to be like a cheap football match.

  25. Re: Here's the video of the landing.Damn it was cl by Dereck1701 · · Score: 1

    Wow, the leg was the only hangup. They were probably so focused on solving what was assumed by everyone else to be impossible, actually landing a nearly empty rocket stage in a predetermined location, that someone failed to do some basic checks/engineering on the one item that everyone assumed would be no problem, some simple landing legs.

  26. Re: Here's the video of the landing.Damn it was cl by Rei · · Score: 1

    SpaceX is nice enough to not hide their engineering development program from us, but you'll note that they keep driving the point home that these are experimental landings. Neither their core business, nor their customers, require them to work. They have dozens of boosters to try with every year, and they're unmanned - they don't have to get it right every time.

    Unfortunately, the only way to truly try out rocket landing.... is to try out rocket landing. It's not like a computer programmer who can just run the program in his test environment numerous times before release, or a car manufacturer who can keep trying out their car systems on private test tracks until the bugs are ironed out. It's not even incremental improvements over earlier rockets in a family that already had most of its bugs worked out in the past. If SpaceX wants to get rocket landing right... they need to land rockets, and learn from that.

    --
    He's the sort of person who would sell the Red Cross to Dracula.
  27. Re:to Land or not to Land, is a secondary question by Rei · · Score: 1

    Indeed. Don't like the result of this launch? Just wait a couple weeks. ;)

    Seriously, that was a beautiful landing. If that leg had latched that rocket would be being offloaded right now.

    --
    He's the sort of person who would sell the Red Cross to Dracula.
  28. Re:4 legs look not very stable. Why not 6 - 8 legs by Anonymous Coward · · Score: 0

    One leg did not lock, she fell over and dented the midsection.

  29. Re:More SpaceX fanboi spin! by rpstrong · · Score: 1

    They were less than two meters off, with good vertical speed. The landing didn't fail; the leg did. How is this not a partial success?