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SpaceX's Grasshopper VTVL takes a 40 meter hop

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Comments

  • Closed Accounts Posts: 4,029 ✭✭✭shedweller


    So no live stream then. Hmph! Ah well, off to bed with me then. I expect great things when i get up.









    And maybe a landed rocket too!


  • Registered Users, Registered Users 2 Posts: 2,537 ✭✭✭thecommander


    shedweller wrote: »
    So no live stream then. Hmph! Ah well, off to bed with me then. I expect great things when i get up.
    And maybe a landed rocket too!

    Live stream of the launch, just not the landing.
    http://www.nasa.gov/multimedia/nasatv/?utm_content=buffer6e91c&utm_medium=social&utm_source=twitter.com&utm_campaign=buffer#.VLDpKsZIiBV


  • Closed Accounts Posts: 2,050 ✭✭✭nokia69


    http://www.spacex.com/webcast/

    should be on youtube too

    weather looking OK


  • Registered Users, Registered Users 2 Posts: 2,537 ✭✭✭thecommander


    nokia69 wrote: »
    http://www.spacex.com/webcast/

    should be on youtube too

    weather looking OK

    And on UStream too. Always good to have a few options, but I doubt there'll be as many watching as usual due to the time in the US.
    http://www.ustream.tv/nasahdtv


  • Registered Users, Registered Users 2 Posts: 30,394 ✭✭✭✭Ghost Train


    must be nearly time for this I guess

    edit 8min


  • Registered Users, Registered Users 2 Posts: 30,394 ✭✭✭✭Ghost Train


    so did the first stage land in the water as was kind of expected, since they keep showing a watery looking video


  • Registered Users, Registered Users 2 Posts: 2,537 ✭✭✭thecommander


    so did the first stage land in the water as was kind of expected, since they keep showing a watery looking video

    The blobs of liquid is the propellant inside the second stage floating around. They put a camera inside the tank.


  • Closed Accounts Posts: 2,050 ✭✭✭nokia69


    Elon MuskVerified account
    @elonmusk Rocket made it to drone spaceport ship, but landed hard. Close, but no cigar this time. Bodes well for the future tho.

    oh well better luck next time


  • Registered Users, Registered Users 2 Posts: 2,537 ✭✭✭thecommander


    Wonder if it went overboard


  • Moderators, Recreation & Hobbies Moderators, Science, Health & Environment Moderators, Technology & Internet Moderators Posts: 92,530 Mod ✭✭✭✭Capt'n Midnight


    http://www.bbc.co.uk/news/science-environment-30752515
    The company CEO Elon Musk tweeted that the booster hit the platform hard.

    "Close, but no cigar," he added. "Bodes well for the future tho'. Ship itself is fine. Some of the support equipment on the deck will need to be replaced." And he continued: "Didn't get good landing/impact video. Pitch dark and foggy. Will piece it together from telemetry and... actual pieces."

    ...
    The barge is less than 100m wide, and all previous experiments had been working on a landing accuracy of some 10km.


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  • Closed Accounts Posts: 2,050 ✭✭✭nokia69


    hitting the barge is pretty good IMO

    they will try again at the end of the month

    I bet they get it right at some stage this year :)


  • Closed Accounts Posts: 4,029 ✭✭✭shedweller


    I wonder what the swell was like? Still though, thats a very good result and bodes very well for the next effort. I cant wait for pics!


  • Registered Users, Registered Users 2 Posts: 2,004 ✭✭✭Hmmzis


    From Musk's tweets it looks like the rocket ran out of hydraulics fluid for the fins, about 10% short. Aparently they use an open system to save weight. Not sure is the fluid is shared with the landing legs' system.


  • Closed Accounts Posts: 4,029 ✭✭✭shedweller


    Hmmzis wrote: »
    From Musk's tweets it looks like the rocket ran out of hydraulics fluid for the fins, about 10% short. Aparently they use an open system to save weight. Not sure is the fluid is shared with the landing legs' system.
    He said there is already 50% more fluid on the next one so theres plenty in reserve.
    They were out by only 10% this time. A simple thing like turbulence or crosswind would have used up the hydraulics quicker. A closed system would have kept on doing its thing but the weight penalty was deemed too much. As usual with rockets, they ride a knife edge and sometimes things go wrong.
    I was actually thinking about the weight thing the other day. Not my weight, the rockets. Given that it will be reusable, wont they have to beef up the structures to cope with metal fatigue? This will be a weight penalty in itself so theres going to have to be a balancing act done with all that. Interesting work!


  • Moderators, Recreation & Hobbies Moderators, Science, Health & Environment Moderators, Technology & Internet Moderators Posts: 92,530 Mod ✭✭✭✭Capt'n Midnight


    *put's on Devils Advocatehat*

    http://www.bbc.co.uk/news/science-environment-30752515
    they would also have to get satellite operators comfortable with the idea of launching their precious hardware on what would essentially be second-hand rockets.

    "The customer doesn't ask for reusability; they ask for reliability at the cheapest cost possible," said Rachel Villain, with the space intelligence company Euroconsult.

    "Reusability is the problem of the supplier, not of the client. A satellite operator has basically three demands - on time, on quality and on price," she told me.

    The launch vehicle weighs 500 tons and has a payload of 1.3%

    India's GSLV Mark III weighs 630 tonnes , and a suborbital test without the finals stages cost $24m ,( the full thing can put 10 tones in to LEO or less than half that to GEO )
    http://economictimes.indiatimes.com/news/science/2014-a-year-of-technological-advancement-for-india-in-space/articleshow/45591930.cms
    so a Payload of 1.6%

    So he non reusable one might be 23% more efficient ?
    But what matters is the cost and reliability.

    Remember some of the SRB segments from the shuttle were reused up to 7 times.


    _80081892_falcon9_dragon_capsule_624in.jpg



    7hHyqnW.png
    from http://www.actmaniac.com/india-to-launch-gslv-mark-iii-satellite-vehicle-by-the-mid-of-december/


    Also http://en.wikipedia.org/wiki/Avatar_%28spacecraft%29


  • Closed Accounts Posts: 150 ✭✭_Jumper_


    Videos of the latest launch are up.


  • Registered Users, Registered Users 2 Posts: 2,537 ✭✭✭thecommander


    Pic of the barge returning to Jacksonville.
    B7F8I4dCMAITxoP.jpg:large


  • Registered Users, Registered Users 2 Posts: 2,004 ✭✭✭Hmmzis


    Looks like there are some bits and pieces on the barge and some minor fire damage. But where is the rocket stage wreck itself, did it fall into the ocean and that on the barge is all that's left?


  • Closed Accounts Posts: 4,029 ✭✭✭shedweller


    Hmmzis wrote: »
    Looks like there are some bits and pieces on the barge and some minor fire damage. But where is the rocket stage wreck itself, did it fall into the ocean and that on the barge is all that's left?
    Looks that way. Those tarpaulins seem to be covering some rockety bits. I really hope the next attempt will be done in daylight so we can see it.


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  • Registered Users, Registered Users 2 Posts: 2,537 ✭✭✭thecommander


    Some serious sleuthing going on over on Reddit. Seems there was a video feed of the landing, only one clip thats cropped out of a tv screen in mission control. It's of the deployed fins. http://imgur.com/ANumpHA

    I reckon we'll eventually see something from the barge.


  • Registered Users, Registered Users 2 Posts: 2,537 ✭✭✭thecommander


    Some images Musk released on Twitter. So close to the landing, but fins gave out at last minute.

    7sUwcIK.jpg

    kKCr4K4.jpg

    qEsgfnw.jpg

    LrwWSd5.jpg


  • Closed Accounts Posts: 2,050 ✭✭✭nokia69


    would love to see the videos

    the 29th can't come fast enough

    I don't think the fins are much help close to the pad, I think they do most of their work higher up where the speed is greater


  • Registered Users, Registered Users 2 Posts: 2,537 ✭✭✭thecommander




  • Registered Users, Registered Users 2 Posts: 2,004 ✭✭✭Hmmzis


    Deeem, that's close.

    Also, the explosion is awesome, can't stop watching the video :D


  • Closed Accounts Posts: 4,029 ✭✭✭shedweller


    Hmmzis wrote: »
    Deeem, that's close.

    Also, the explosion is awesome, can't stop watching the video :D
    It fairly chucked the top overboard eh?!
    One thing thats bothering me. It was coming down very fast and how much of this is due to the loss of steering?
    Because if it was doing that speed in an upright position it would have ended badly anyway.
    They've done this on dry land anyway so im confident for the next effort.
    We need more of this awesomeness!


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  • Registered Users, Registered Users 2 Posts: 2,537 ✭✭✭thecommander


    shedweller wrote: »
    It fairly chucked the top overboard eh?!
    One thing thats bothering me. It was coming down very fast and how much of this is due to the loss of steering?
    Because if it was doing that speed in an upright position it would have ended badly anyway.
    They've done this on dry land anyway so im confident for the next effort.
    We need more of this awesomeness!

    It's like when you balance a brush handle on your hand, once you go beyond a certain point of it tipping it's gone. Combine that with engines that are still lit and it will accelerate in that direction. I think the speed was fine, just the tipping threw it. We'll see next time.


  • Registered Users, Registered Users 2 Posts: 2,339 ✭✭✭The One Doctor


    Does SpaceX user vernier engines for landing the first stage? It'd save them a lot of faffing around if not.


  • Closed Accounts Posts: 4,029 ✭✭✭shedweller


    Now that i have looked at it again it does look like its coming towards the camera which would explain its high vertical speed.
    They better do the next one in daylight and with a handful of go-pros!


  • Closed Accounts Posts: 2,050 ✭✭✭nokia69


    shedweller wrote: »
    It fairly chucked the top overboard eh?!
    One thing thats bothering me. It was coming down very fast and how much of this is due to the loss of steering?
    Because if it was doing that speed in an upright position it would have ended badly anyway.
    They've done this on dry land anyway so im confident for the next effort.
    We need more of this awesomeness!

    my guess is that when they lose the fins, the engine had to over compensate during the last burn


  • Closed Accounts Posts: 2,050 ✭✭✭nokia69


    Does SpaceX user vernier engines for landing the first stage? It'd save them a lot of faffing around if not.

    cold gas trusters AFAIK


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  • Registered Users, Registered Users 2 Posts: 2,004 ✭✭✭Hmmzis


    shedweller wrote: »
    It fairly chucked the top overboard eh?!
    One thing thats bothering me. It was coming down very fast and how much of this is due to the loss of steering?
    Because if it was doing that speed in an upright position it would have ended badly anyway.
    They've done this on dry land anyway so im confident for the next effort.
    We need more of this awesomeness!

    It certainly solves the mystery of the missing bits (well, most of the stage actually). If the hydraulics failed with a minute to go then that's fairly high up still. The gimball of the engine apparently wasn't enough to balance out the stage. My understanding is that only a very limited deviation from vertical can be controlled by gimballing engines without adding excessive horizontal velocity.


  • Registered Users, Registered Users 2 Posts: 2,537 ✭✭✭thecommander


    Does SpaceX user vernier engines for landing the first stage? It'd save them a lot of faffing around if not.

    No need for them, would add far too much weight swell. They've shown with the grasshopper tests and CRS5 landing that they can get to a point without them. Not enough hydraulic fluid was the problem, once they have enough I'd be certain enough they'll land it (unless some unknown issue arises)


  • Closed Accounts Posts: 4,029 ✭✭✭shedweller


    I was just thinking. The extra hydraulic fluid is going to weigh more. How would it compare to having a return line to the hydraulic pump and reuse a smaller amount of hydraulic fluid? Like a normal hydraulic system.
    Ok, this would require an in depth knowlege of the rocket to give a definite answer but still, there's some merit in that surely?
    And i know there would have to be extensive re-testing done. But it would mean the controls will stay working no matter what.
    Anyway, i had to ask. I dont like seeing machines breaking down!


  • Registered Users, Registered Users 2 Posts: 2,537 ✭✭✭thecommander


    shedweller wrote: »
    I was just thinking. The extra hydraulic fluid is going to weigh more. How would it compare to having a return line to the hydraulic pump and reuse a smaller amount of hydraulic fluid? Like a normal hydraulic system.
    Ok, this would require an in depth knowlege of the rocket to give a definite answer but still, there's some merit in that surely?
    And i know there would have to be extensive re-testing done. But it would mean the controls will stay working no matter what.
    Anyway, i had to ask. I dont like seeing machines breaking down!

    If you have a closed loop you need pumps which add weight and complexity. They use pressurised gas to pump the fluid out, seems to be a case of just adding more fluid (and more gas I guess)


  • Moderators, Recreation & Hobbies Moderators, Science, Health & Environment Moderators, Technology & Internet Moderators Posts: 92,530 Mod ✭✭✭✭Capt'n Midnight


    If you have a closed loop you need pumps which add weight and complexity. They use pressurised gas to pump the fluid out, seems to be a case of just adding more fluid (and more gas I guess)
    Actually it's cleverer than that they reuse the fluid in the engines because it's fuel.

    There's a lot to be said for using simple reliable systems even if they are slightly heavier. Complexity adds risk. And given the % of spaceflight failures shaving off too much weight on stage 1 is just asking for trouble.

    http://space.stackexchange.com/questions/7771/why-does-the-falcon-9-consume-hydraulic-fluid
    Falcon 9 uses an open hydraulic system that has a separate tank of RP-1 (which is used as the hydraulic fluid) pressurized by Nitrogen near the interstage, which, after use, drains down back into the main RP-1 tank for "reuse" by the engines. There are a variety of reasons that SpaceX made decisions to use this design:


  • Closed Accounts Posts: 4,029 ✭✭✭shedweller


    I must humbly hang my head in shame for not thinking of that...
    D'oh!


  • Registered Users, Registered Users 2 Posts: 2,537 ✭✭✭thecommander


    Complexity adds risk.

    Exactly. So don't use more pumps.


  • Registered Users, Registered Users 2 Posts: 9,529 ✭✭✭irishgeo


    Is it supposed to land on the barge horizontal or vertical.


  • Closed Accounts Posts: 4,029 ✭✭✭shedweller


    irishgeo wrote: »
    Is it supposed to land on the barge horizontal or vertical.

    Vertical. Wouldnt want to be much swell in the sea when it lands!


  • Closed Accounts Posts: 150 ✭✭_Jumper_


    Google and Fidelity Investments have bought just shy of 10% of SpaceX, plan to pump money into helping it develop Satellite Internet for undeveloped/underserved regions around the world or in Musks case, beginnings of Internet for Mars Colony.

    Values SpaceX at 10 Bil Dollars.

    Valuations be crazy.


    What would be a good name? Hmm, Trans Net?


    gigaom.com/2015/01/19/elon-musks-satellite-plan-project-loon-without-helium-or-latency/

    bloomberg.com/news/2015-01-20/musk-s-spacex-sells-10-stake-to-google-fidelity-for-1-billion.html?hootPostID=e032d9a22131660ad2c3ecfaa1639a46


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  • Closed Accounts Posts: 2,050 ✭✭✭nokia69




    can't wait to see this badboy fly


  • Closed Accounts Posts: 2,050 ✭✭✭nokia69


    http://en.wikipedia.org/wiki/Deep_Space_Climate_Observatory

    possible spaceX launch tonight, just after 11

    they will also try first stage recovery again but it will be harder than the ISS missions, so who knows if it will work

    you can watch it at http://www.spacex.com/webcast/


  • Registered Users, Registered Users 2 Posts: 2,537 ✭✭✭thecommander


    Tomorrow so!


  • Registered Users, Registered Users 2 Posts: 2,285 ✭✭✭MayoForSam


    Now happening at 10:45pm tonight (live webcast).


  • Moderators, Recreation & Hobbies Moderators, Science, Health & Environment Moderators, Technology & Internet Moderators Posts: 92,530 Mod ✭✭✭✭Capt'n Midnight


    now showing live feed


  • Registered Users, Registered Users 2 Posts: 1,651 ✭✭✭greedygoblin


    No go? :(


  • Moderators, Recreation & Hobbies Moderators, Science, Health & Environment Moderators, Technology & Internet Moderators Posts: 92,530 Mod ✭✭✭✭Capt'n Midnight


    high altitude winds so tune in again tomorrow at 23:00


  • Registered Users, Registered Users 2 Posts: 2,004 ✭✭✭Hmmzis


    aaand it's a scrub - 151% violation of high altitude winds if I heard the comms right.


  • Registered Users, Registered Users 2 Posts: 1,557 ✭✭✭Knifey Spoony


    Looks like they won't be attempting recovery of the first stage using the drone ship due to weather in the Atlantic. :(

    There'll be a soft landing in the water instead.

    http://www.spacex.com/press/2015/02/11/dscovr-launch-update


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  • Closed Accounts Posts: 2,050 ✭✭✭nokia69




    falcon 9 first stage on the road to the cape, might be for CRS 6


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