DARPA Proposes Ripping Up Dead Satellites To Make New Ones
Hugh Pickens writes "DARPA reports that more than $300 billion worth of satellites are in the geosynchronous orbit, many retired due to failure of one component even if 90% of the satellite works just as well as the day it was launched. DARPA's Phoenix program seeks to develop technologies to cooperatively harvest and re-use valuable components such as antennas or solar arrays from retired, nonworking satellites in GEO and demonstrate the ability to create new space systems at greatly reduced cost. However, satellites in GEO are not designed to be disassembled or repaired, so it's not a matter of simply removing some nuts and bolts, says David Barnhart. 'This requires new remote imaging and robotics technology and special tools to grip, cut, and modify complex systems.' For a person operating such robotics, the complexity is similar to trying to assemble via remote control multiple Legos at the same time while looking through a telescope."
This sounds like one of those brilliant ideas on paper, but one that will prove infinitely harder in reality. Re-use satelites, great idea, good luck doing it though.
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Would the whole process and those dated components even warrant all those expenses?
Man, if only someone could design a launch vehicle which could also be used to capture and return old satellites to Earth for disassembly. Although knowing how these things work I suspect such a vehicle would never really be used to it's full potential and become retired shortly before someone else noticed it might be a good idea.
I thought non-functioning satellites were kicked into a higher orbit so their slot could be reused.
As far as the idea of reusing component, I just have the thought of instead of one big piece of junk in a stable orbit turning into lots of components in unstable orbits.
Earthbound junkyards work, because there's lots of interchangeable parts that can be harvested from old cars. Can the same be said of satellites, or are they made of one-time built to order parts? Also, it's one thing for a junkyard part in your car to crap out on the road. Do you want to trust satellites in orbit with used parts? Oh, just stop by the orbital junkyard, for a new used part . . .
Schroedinger's Brexit: The UK is both in and out of the EU at the same time!
The Pentagon is making it and they are not known for being green. So the actual purpose could be as a weapon against other satellites.
We could just bring them back to earth and relaunch them later. Now all we need is a space craft that can land on earth after a trip into near orbit...
Watch those corners
Who does an old defunct satellite belong to? I suspect that it still belongs to whoever put it up there, or their executors, whoever bought the company etc.
And who is authorised to say that something is defunct anyway? Imagine such phrases as "We left it dormant for future needs." and "We were keeping it until we could go up ourselves, collect it, bring it back and repair it."
Scientists and engineers may have worked out the economics of doing this, but have they included that nasty concept of Corporate Lawyers?
I'll see your Constitution and raise you a Queen.
Arrgh, what is it with slashdot posters, there is no such thing as Logo's, just like you don't say multiple USB's, you say multiple USB Ports. Lego is the brand name for the construction system and the components are called bricks or components, so the correct way to say this would be 'multiple Lego bricks' or 'multiple Lego components'.
Why hasn't there been a Republican backlash over this? This is clearly a case of "reuse", which is one of the 3 Communist Rs (the others are "reduce" and "recycle").
It seems to me that ownership issues would be a major concern. Say corporation A and corporation B send up satellites at the same time. Both have components break in the same year, rendering both satellites useless. However, since 90% of each satellite is still usable and since the components are on the other satellite, it makes sense to cannibalize one for the other. Which one gets cannibalized? Who owns the final frankenstein?
Any VC's out there want to start a business with me? Buy up dead satellites for pennies and sell them to DARPA or become the space scrap yard. PM me if interested!
one of the primary drivers of the high cost is the launch costs,
It's interesting todo because the antennas and solar panels makes up quite a lot of the launch costs... they're not talking about reusing everything, just the heavy parts :)
As the article says, the current birds are not made for this, and that is one orbit that you really don't want to play Angry Birds in. It would make much more sense to mandate that if you want GEO orbital space any new satellite would have to be highly modular and repairable, and maybe even plan for refiling (although if you think fuel is expensive here just wait to see the cost there). With an insane amount of money you might kluge together something with the current scrap, but I doubt it could offset the cost of getting the robots to do it there in the first place. Far better and safer to cut losses on the old junk and stop sending up unfix-able designs.
I'm an American. I love this country and the freedoms that we used to have.
It sounds suspiciously like these satellites are products made by Apple.
Is this DARPA's real motive or do they want the ability to cannibalize enemy satellites?
A huge orbiting junk yard could lead to a space-station, the Chinese could build this and make a permanent step into space and help clean up all of the orbiting space junk, of which their must be millions of pieces by now. That would make future trips into space much safer.
We can only hope.
liberare massarum ex ignorantia, clausa descendit molestie.
We sorta have one in the X-37. No idea if it is big enough to haul a satellite, or if it even has a robotic arm capable of catching one.
I believe they are looking for new missions for this spacecraft to justify continue development. Perhaps the reason for the suggestion? They are currently proposing a "C" model that is 20% larger to provide the capability to haul astronauts in the cargo bay.
http://en.wikipedia.org/wiki/Boeing_X-37
You forgot that part.
Um, maybe the reconstructed satellite will want to mind meld with a bald Asian sex goddess?
I thought that the cost of bringing the satellite into space exceeds the cost of the actual hardware a lot. Does it really make sense to harvest the parts? I'd like to see numbers.
rip up the government and make a new one instead
Screw developing more robots, although robots are cool, but this is THE REASON to send real-live Union Labor to do the job.
DISCLAIMERS:
- Though not hostile to the US, I'm a foreigner, so don't expect me to hold your hands, too.
- Overall, I tend to consider everyone first as Earthlings, then humans and finally as citizens of a country.
- Defense usually means reacting. It seems to mean "attacking" in English (IMHO "wake up first and kill him before he kills you" is apelike, not human).
We need some kind of agreement for space like the one we have about Antarctica.
That before you recycle another country's satellite and this makes them angry; part of the Defense goals is to avoid stepping on the toes of others. Avoid creating enemies: it's way cheaper than fighting them.
Having power is great, but it's worthless without control.
We were made to have limited powers and so, until now, the world has not been destroyed. Limit yourselves before you regret having too much power.
http://www.imdb.com/title/tt0064691/
Actually, a reusable space plane would be real handy for this kind of job.... oh, wait.
A lot of reactions talk about the cost of fuel... seemingly these people forget that the satellite in question might still have fuel available that is going unused. What if out of this research it becomes clear that any new satellite needs the requirement to have enough fuel left for one last journey to the collector satellite orbit where it will be dismantled.
I wonder how a slashdot story about Darpa seeking input on a research project for some kind of network that can route around damage would be received. Seems like Slashdot is getting more and more users that immediately go negative rather then exploring the possibilities.
MMO Quests are like orgasms:
You may solo them, I prefer them in a group.
This sort of thing could really put a space station and its inhabitants to easy to understand use, fix and repair stuff in orbit. Keep most of the kinetic energy, get unobstructed sunshine, and catch some space junk - campy. Running a solar sailing race on the side as a hobby could be entertaining.
I remember that there existed a TV show about junkyard people in the past. Maybe one could come up with a space comedy around it. Some cross between Alien and Space Cowboys maybe.
Je me souviens.
I made some comment about the topic in the past. Nice, DARPA listened, or to be more modest, had a similar idea.
Darn sad I can't find it now. Thinking about it, it really isn't that hard to come up with the idea, somebody like Oberth or Ziolkovsky probably already thought about it.
Je me souviens.
if they can prove reassembly in orbit is viable then it suggests that the space industry needs to standardize to facilitate this.
* Winners compare their achievements to their goals, losers compare theirs to that of others.
I have this perfect idea. We build a re-usable re-entry vehicle that allows us to launch new satellites, and while in orbit we could retrieve the defunct older satellite and simply bring the whole thing back to Earth. Then when the satellite's on Earth we can scrap the heck out of it, re-using nearly everything that's in it in the first place. Maybe even just replace that one pesky component that failed, re-test everything and send it back up on another mission.
I envision this space vehicle to have a huge cargo bay capable of taking heavy loads into orbit, maybe we could even use it to build and re-supply the space station. It would would re-enter the Earth's atmosphere and then act like a glider of sorts to land on a conventional runway. The payload would be removed and the orbiter prepared for another mission in less than a few weeks.
This could be the best solution out there as it gets the old piece out of orbit thereby nullifying it's danger to other orbiting objects; allows us to recycle the valuable components and progresses human exploration of space.
In fact, I know where there are about four of these very spaceships just waiting to be used. ... all sarcasm aside, the Air Force B-52 was developed in the 40's and is STILL flying today, even after follow-on fighter/bombers were developed, deployed and are now retired. There may have been a lot of things wrong with the Space Shuttle, but there were far more things -right- about it that it should have been brought into the 21st century and continued service. No, I don't work for NASA, but I've been a fan of the space program since I was a little boy.
And it's beautiful Canada Arm.
Use some of those inflatable habitats and build a dry dock / junk yard in orbit. Use a tug to take stuff back and forth to and from LEO and GSO.
Undetectable Steganography? Yep, there's an app fo
The ISS is expensive to keep in operation with a crew, so there has been discussion of taking it out of service in a few years, and de-orbiting it. My suggestion is to salvage it using robotic technology, and use the material to build new satellites in space.
The original space program had enormous technological benefits for society that would have been valuable even if we had failed to land on the moon. I believe a program to develop robots to disassemble the ISS and build satellites would also pay dividends in terms of advancing robotic technology for manufacturing and recycling, whether the goal is achieved or not.
...and you didn't want to wear your older brother's patched jeans to school?
Now - under the expert leadership that contaminating politics with money yields - the space program of the United States of America is going to wear patched satellites in outer space...that's progress.
Orwell: "In a Time of Universal Deceit, telling the Truth is a Revolutionary Act"
".. the complexity is similar to trying to assemble via remote control multiple orbiting Legos at the same time while looking through a telescope."
Fixed that for you.
The three laws of thermodynamics:(1) You can't win. (2) You can't break even. (3) You can't even quit.
So where does Solid Snake fit into all of this?
Most satellites have essentially no situational awareness, because being taken apart by little aliens in shiny green spacesuits (or by advanced remanufacturing robots) is just not part of the threat model. So it tends to be very hard for ground control to distinguish between a random equipment failure and a failure caused by deliberate modification of the spacecraft.
This mission probably isn't what the X-37 is for, since it's a low earth orbit vehicle, not geosynchronous.
MOVE THE FUCK ON ALREADY
Return to Earth ? Are you a fucking retard ? Did you miss the whole fucking point ?
A sort of suicidal hunter-killer micro bot bird flock. Launched with scores of these bots in each rocket, on attaining orbit they spread out, attach to dead junk and deorbit it. Or aggregate it all in one spot for this proposed mechbot to service.
Help stamp out iliturcy.
If one component is failed, why not replace it? The reason we don't do that now is that it's a complicated operation to do in space but if the point is to develop the technologies to make this kind of salvage possible, wouldn't it be just as easy to replace the broken part in some cases?
Of course the ONLY value these parts have up there is that they are already up there. Bringing them back would make absolutely no sense at all, since that would destroy the only value they have.
Wouldn't this technology also allow working satellites belonging to others to be "harvested"?
..either. Retry your argument.
There are definitely issues to work out, but the costs involved with getting one pound of anything into space is incredible. Once you get it there, if you can figure out how to recycle it and keep it there, there are definitely savings to be had (and therefore... money to be made). A current 3D printers would require some gravity, but get past that and just about anything plastic can be recycled. How about some kind of solar furnace and aluminum? I'm in. Let's do it. :-)
There's no need to rush. Solar sails can move Mr. Fixit from one spot to another. Or Mr. Fixit can attach a sail to junk, and program the sail controls to take the junk to a junkyard (a.k.a. the moon).
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Although those bits are fast they are not large. If it comes down in a major city it's not going to do as much damage as a light plane coming down at speed and it's going to be easier to find the radioactive bits than in a remote area. Remember that even fairly weak sources of gamma rays are very easy to detect. Would it even give one person cancer before they get away from it? They'd have to be pretty unlucky or ignore the likely evacuation order.
Take a look at wikipedia or elsewhere for these devices. They are not large. A lot of them are just a small photon source and a photovoltaic.
Also people tend to panic a lot less in real disasters than in disaster movies. Two towers down and fear of more terrorist attacks did not result in a lot of people stomping their fellow man to death to get out of New York.
I'll try to put things more clearly. If you are going to change your path of movement to that of another object you not only have to get there but also match speed and direction with the other object. That means at least two changes. :) Maybe think of it in terms of gliders flying parallel to the ground and you need to get from the one in front to the one behind. If gravity could be ignored they wouldn't stay in orbit anyway.
Your "just drop down to a lower orbit" means a change in speed so an expenditure of fuel. Once you have the right position "below" as you suggest (which it won't be because it's not a stable orbit, in fact the altitude would still be around geostationary) it's then another burn to get to the object you want to match orbits with and then another to slow down and match the orbit. That's not going to be a trivial expenditure of fuel unless the distances are trivial. If it's 180 degrees away waiting a long time isn't going to solve the problem because gravity is making it harder to get back into geostationary orbit with every passing second.
You have think about it in two dimensions of polar co-ordinates instead of just one
Yeah, but the law doesn't.
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(Ignore the underscores, spaces get formatted out and the junk filter hated my version with dots showing the arc.)
Once you get there you need another burn to speed up and have the right heading.
All this of course takes fuel. For major changes in angle it takes more fuel than minor changes. You can't just "get off the wheel", wait, and then climb on again. There's nowhere else to stand.
There are lots of things the law doesn't allow that governments and the military get away with.
Ok, what if you say, rendezvous with the satellite harvester, except you overshoot by a few km/s
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No you don't - with respect you are not even grasping the concept of rotation and are only thinking of fixed circles which is why I'm trying to describe it to you in a more familiar set of 2D co-ordinates. It's not a silly single dimension idea of concentric rings of wheels, there is a second dimension. You don't just step from one orbit to another without passing through intervening space and in fact you would never want to if you just want to shift to a different angle at the same altitude. Instead you completely leave the circle and go for an arc that would be slightly elliptical if it was to be a complete orbit - there is no need to waste fuel moving into a different circular orbit and getting out of it again (4 burns with your idea if you think about it - you can't get the change in velocity for free).
Even with just two burns with that arc that would become an ellipse it's not going to be trivial amounts of fuel for large changes in angle. The greater the divergence the greater amount of fuel you've got to burn at the start and finish. Even if you don't care if it takes 100 intersections of the two paths to get to the end point you still lose something - gravity is making the angle between the two diverge a bit with every orbit and in the end you've got to burn fuel to get back on that circular track. The longer you "wait" the more fuel you need to burn to correct it at the end. There is nowhere to step off and no free ride anywhere apart from down.
No no no - the situation here is moving around in the same orbit to do things with satellites in geostationary orbits. What you are describing is to move from one orbit to another - read the web page. :)
You could move to another circular orbit, stabilise in and then move back up again - which seems to be what you are suggesting - but that would take four burns and you don't need to do it, space has more than one dimension guys! It doesn't just have be a ring of circles numbered one to whatever. Things can move at angles as well and there are elliptical orbits.
As for microgravity that's all relative within objects in space but the orbiter is going to be influenced by a really big mass that is relatively close - take a look at Newtons law of gravitation that you seem to have temporarily forgotten
The first thing I thought of was the Military chopping bits off other country's satellites, and then a maybe Star Trek episode with a rogue robot wandering the galaxy cannibalizing stray hardware, slow-moving starships, &c.
They feared that it could be used to suppress protest or support unpopular rule.
Things can move at angles as well and there are elliptical orbits.
What else do you think a Hohmann transfer is?! An elliptic orbit that lets you move from one circular to another.
If you're suggesting altering the plane of the orbit though, that'd take a massive amount of propellant and completely pointless.
you are not even grasping the concept of rotation and are only thinking of fixed circles
What, you're reading my mind now? Fixed circles? what gave you that idea?
You don't just step from one orbit to another without passing through intervening space
If you're in a circular orbit, simply increasing or decreasing your velocity will put you in an elliptical orbit with perigee or apogee at your current position. If you're in an elliptical orbit, increasing your velocity at apogee or decreasing your velocity at perigee can put you in a circular orbit.
there is no need to waste fuel moving into a different circular orbit and getting out of it again
It's not wasting fuel. Fighting gravity is wasting fuel.
(4 burns with your idea if you think about it - you can't get the change in velocity for free)
The amount of propellant expended has nothing to do with the number of burns. It has everything to do with the total change in velocity, which is about 10m/s for a 100km difference. In reality, you can get away with a lot less than that.
it's not going to be trivial amounts of fuel for large changes in angle.
That's why no one does that. Satellites don't even have enough thrust to do that.
...no free ride anywhere apart from down.
Ok, I think I've got it. This is wrong, There's no free ride anywhere, not even down. If you're not going fast enough for a circular orbit at your altitude, you are pulled toward the earth by gravity. Your altitude is falling, but your velocity is increasing. Eventually you reach a point where your velocity is too high for a circular orbit at your altitude, and you go flying out into space again. This is an elliptical orbit. The ellipse isn't centred on the earth, the earth is at one of the foci.
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No, reading your posts where you have made that extremely obvious. If you can't understand what I have below go find a first year engineering or physics student or a bright high schooler to sketch you up some diagrams because it's hard to get you from nowhere to somewhere without diagrams.
It's more than that because it is happening in two dimensions.
Angular velocity and radial velocity and you don't get from A to B by magic - you get there by motion. That requires expending extra energy.
No you don't because you don't have to stick to a circle - there are other arcs that can intersect that circle and there is more than one dimension. I'm sure you know this but I'm writing it just in case you don't so please don't get offended, and I should have really written this in the reply to the other guy that is a bit furthur behind. A one dimensional description has position only in terms of altitude and only angular velocity, and some people leave school thinking that's enough and satellites hop from one circular orbit to the next. That's not enough to describe moving around an orbit. You need to be able to consider radial velocity in addition to angular velocity. That is what I meant when I tried so many times to point out the mistake by writing that it's not a 1D problem.
You've got that right and so will staying on the same plane and changing the angle around the orbit. You don't get that for free no matter how long you wait or what course you are on.
I get the impression you've forgotten about what the article summary was about since you keep going on about transfers to a different orbit:) It is about moving around getting bits off geostationary satellites to do repairs or build new ones.
But this is NOT about doing that and is about a different change in location.
Just as well the article wasn't about a skip trajectory. I'm amazed how long this thread has got with something this simple.
Sorry to reply again, but you'll probably see what I mean best if you draw some circles and ellipses on a sheet of paper. Each change in direction costs fuel so you'll see what I mean about two changes instead of the four you'd need to do two Hohmann transfers with everything else equal (same burn angle and time).
What I'm trying to get across is that it isn't easy to move around an orbit and the method you've suggested makes it twice as hard as it could be.
I had a similar idea way back when they announced they were retiring the shuttle....so I mentioned maybe letting it do one last up, but not a down, and leave it in space for parts that could be used for future projects needing materials etc.... but was found by most to be idiotic with this type of thinking, yet here we are many years later with a similar idea about satellites...which to me makes perfect sense....however I will say what someone else told me....
The satellites are old technology and probably do not contain anything worth salvaging, ....but my true feelings are that any type of material can be useful for fixing stuff, not just creating stuff....so why not???
Radial and Angular velocity are two ways of writing THE SAME THING, just in two different coordinate systems (polar and Cartesian respectively).
You seem to think that four small burns will take up more fuel than two large burns (to move in and out of the ellipsoid you're proposing would take LARGE burns). The reason I keep going on about 'transitions to a different orbit' is because every time you thrust, you're transitioning to a different orbit. The orbit may or may not be circular or stable, but it is an orbit. There is no 'just changing locations in an orbit', orbital motion does not work like that. Moving about efficiently is all about picking the orbits with the lest amount of energy needed to move between them. It takes LESS energy to move from GEO, via a Hohmann orbit, to a sub-GEO orbit, via a Hohmann orbit, and back to GEO, than it does to thrust into an elliptical and than back to GEO in one go. The reason is simple: the elliptical will have a large difference in eccentricity, so circularising would take a lot of propellant. Hohmann transfers are, by definition, the orbit with the smallest difference in eccentricity between two orbits.
But you don't need to take my word for it: look up every satellite launch ever performed within Earth orbit: all move around via Hohmann transfers. NASA, JAXA, the ESA, Roscosmos, and everyone else, don't do that for shits and giggles; they do it because it's the most efficient way of moving about using chemical propellants.
Sorry that was a typo - I meant the radial and perpendicular components of the angular velocity. In this thread there seems to be a lot of ignorance that there is anything other than the perpendicular component. (Also they are not the "same thing" unless there is no perpendicular component). Anyway, without considering both there's no way to actually understand the situation, only pretending to understand by mentioning terms that sound sortof as if they might fit if you repeat them enough.
As I said above they are moving to a different place to what we are discussing. It looks like you've just found the first thing that mentions orbits and assumed it fits in all cases. :) The radial component would be just enough to counteract gravity for the time needed to get to the right angle - slower so you drop faster and have to climb at some point if you want to get back to the same orbit.
I also suggest you get that pencil and paper and look at that Hohmann transfer again, plus I sould have put with everything else equal (same burn angle and time) in bold so you would have noticed it last time. Your "the elliptical will have a large difference in eccentricity" is not necessarily correct - it's just hard to draw it with ASCII art otherwise and still be readable
You are almost there - you wrote "circularising would take a lot of propellant" but for some reason have yet failed to understand that you do that TWICE with your suggestion which is why it is a bad idea.
To get from one point on an orbit to another point on the orbit you can both slow down and oppose the acceleration due to gravity by going "up" and getting pulled "down" over time after the burn.
I didn't want to do the math, but I suppose it's the easiest way. Ok, you thrust to reduce velocity and thrust upwards to compensate for gravity pulling you down. The length of GEO is about 265,000km. If you slowed yourself by 5m/s (half of my rather extravagant budget) it would take 307 days to go 180 degrees. That's 307 days you have to accelerate an average of 1.456 x 10^-3 m/s^2 away from the earth for a total of 38.62km/s. This is enough for a mars landing and back. Add another 5m/s to get back up to speed. If you don't thrust away from the earth, gravity pulls you down. This isn't a problem, because when you thrust to speed up again, you'll come right back up. Again: -2.5m/s to go into an elliptical orbit, -2.5m/s again at perigee to go into a circular orbit at GEO - 100km, wait until you're 1/2 orbit from where you want to be, +2.5m/s to go into an elliptical orbit and at apogee you will be exactly were you want to be, going in the direction you want to be going, and 2.5m/s too slow. +2.5m/s. So your choice: 38,630m/s or 10m/s?
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Wow. You really need to sketch it out on a sheet of scrap paper to visualise what is going on if you are getting that sort of result :) Accelerating all the way back? WTF? You can go up and down instead of staying on the one dimensional circular track which is what I've trying to point out all of this time. WTF do you think you do to start a Holman transfer? It's not a magic trick to jump from one location in one dimensional space to the next - it's a movement in two dimensions and there can be other movements in two dimensions and other things you can do with non-circular paths.
:( It appears you only get simplistic bullshit about a mass on a string and teen arrogance taught instead of anthing useful.
I'll see if I can explain things a bit more clearly. For 180 degrees you don't have to hit it on the first pass. No Holman transfer needed - that first little kick DOES put you into an elliptical orbit it was just that I was showing the first part of the arc that makes up an ellipse if it does a full orbit. If the first intersection doesn't get you there one later on will, but of course as time progresses gravity is pulling you down a little bit with every orbit that you are doing less than the stable speed at GEO. When you get to the right angle you then accelerate in the transverse direction and cancel your radial velocity to properly get back into GEO. Say if you start with a 2 degree "hop", that's 90 orbits (or maybe less since the incident angle between the ellipse and circle will change as gravity just keeps on accelerating you towards the ground) to get to 180 degrees and probably not a huge amount of time so probably not a huge increase amount of radial velocity change from gravity. It's hard to describe, but if you sketch it you'll probably grasp it almost instantly.
As for the choice - obviously neither and sadly your 10m/s is wrong as well because you are ignoring the radial compenent of getting in and out of the elliptical orbits to move!!! 2D problem! Why are you guys not listening when I keep repeating that over and over and also convinced that you are correct without going anywhere near the mathematics?
Anything with rotational motion or conic sections really seems to confuse people without any background in engineering or physics
...when somebody mangles "It's not heart surgery." and "It's not rocket science." into "It's not rocket surgery." anymore.
Orwell: "In a Time of Universal Deceit, telling the Truth is a Revolutionary Act"
You can go up and down... ...WTF do you think you do to start a Holman transfer?
You accelerate perpendicular to gravity. Here, read This. Look at the diagram.
I should have done the math properly: To move from GEO to GEO - 100km, you need:
sqrt(earth geopotential/42164km)*(sqrt(2*42064km/(42164km+42064km))-1) = -1.8257 m/s and
sqrt(earth geopotential/42064km)*(1-sqrt(2*42164km/(42164km+42064km))) = -1.8268 m/s
To get back to GEO you need
sqrt(earth geopotential/42064km)*(sqrt(2*42164km/(42164km+42064km))-1) = +1.8268 m/s and
sqrt(earth geopotential/42164km)*(1-sqrt(2*42064km/(42164km+42064km))) = +1.8257 m/s for a total delta-v of 7.305 m/s.
404: sig not found.
You are still only doing it as 1D - that's like trying to find the area of a circle using a single triangle and is never going to work. Read the bit under "explantion" and then consider that time while moving and in the lower orbit matters because gravity hasn't gone away.
This may at least make you think you understand: imagine a Holman transfer, now imagine putting it on a slight angle to go up a bit and instead of going to a lower orbit ending up on the same one. For large changes you might go around a few times just like the shuttle did getting to orbits at different heights doing an actual Holman transfer (ever notice they sometimes took a day or so to get there instead of minutes - they went around a few times to save fuel). So like a Holman transfer only different (or in other terms, an ellipse). It's just swapping the simplist case which does not fit for a slightly different variant. Happy now?
Anyway, maybe from your 1D attempt at considering a 180 change by decellerating back to zero velocity (which by your 1D model would then put the object in the centre of the earth) you might have got a bit of a rough idea that moving around in the same orbit is not so trivial as a poster suggested a long way above. All we need now is an online physics textbook that can take you through step by step until you can actually understand what a Holman transfer is instead of just bringing it up as if it's a magical incantation. There's no point linking it like above and pretending it's the answer to anything until you've read through it and understand it.
You are still only doing it as 1D
I'm ignoring you when you say this because otherwise I'm forced to think you are crazy.
that's like trying to find the area of a circle using a single triangle and is never going to work.
I have no idea what this is supposed to mean.
Read the bit under "explantion" and then consider that time while moving and in the lower orbit matters because gravity hasn't gone away.
Still don't know what you are saying here. There are only two thrusts in a Hohmann (note spelling) transfer and in the ideal case they are assumed to be instantaneous.
... and instead of going to a lower orbit ending up on the same one.
You're going to do better than this. If you accelerate in any direction you are in a different orbit.
Anyway, maybe from your 1D attempt at considering a 180 change by decellerating back to zero velocity (which by your 1D model would then put the object in the centre of the earth)...
Where did you get this? The relevant line is "If you slowed yourself by 5m/s..."
...you might have got a bit of a rough idea that moving around in the same orbit is not so trivial as a poster suggested a long way above.
That's why it's stupid and no one does it. You transfer to a different orbit and wait for the right phase.
...actually understand what a Holman transfer is instead of just bringing it up as if it's a magical incantation.
I know what a Hohmann transfer is. You can't even spell it. Go read it again. Come back when you get it.
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May I also point out that the article is about getting to satellites located at different points in a single orbit.
That really puts your "Come back when you get it" in a different perspective doesn't it?
Now I suggest actually reading some of things I've written above and other things on the subject and you may get a glimmer of a clue why I wrote that it's not trivial in terms of fuel to move to another location in the same orbit. Don't ignore the 1D comment and get insulting about it because it tells you where your mistake is which is why I've kept repeating it in the hope it will sink in.
We are not talking about a weight on a string going around in a circle but instead about orbital transfers. The simplist case you could find does not fit because it doesn't address anywhere near the actual problem - for instance it ignores time and the suggestion that you just "wait" in a lower orbit depends upon time for it to work! Of course if you ignore time any extra fuel costs due to gravity working on the object over time also get ignored which makes it a useless model that will give very unrealistic results and make the model look very attractive to those that do not understand what the model is supposed to represent.
I can't be thinking in one dimension. Circles and ellipses don't exist in one dimension.
Of course if you ignore time any extra fuel costs due to gravity working on the object over time also get ignored...
There are no "extra fuel costs." Where did you get that idea? Better question: what do you think would happen if I waited forever?
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In polar co-ordinates a circle is defined by only it's radius (1D) while a point is defined by radius and angle (2D). Now do you get it? The problem is changing angle and thus not solvable in 1D, and is also dependant upon time. :(
Your unjustified arrogance is getting more depressing with each indication that your ignorance is deeper than expected
Unless energy is expended to maintain the forward velocity the orbit will decay into an elliptical orbit and the satellite will eventually fall to earth. The higher it is the less acceleration towards the ground there is due to gravity and the longer it will take for the orbit to decay to a given point. Now do you see why time matters and why altitude (radius) matters?
In polar co-ordinates a circle is defined by only it's radius (1D)
Define an ellipse using only one number.
Your unjustified arrogance is getting more depressing with each indication that your ignorance is deeper than expected :(
I was thinking this about you, but I wasn't going to say it.
Unless energy is expended to maintain the forward velocity...
There's drag in space now? News to me.
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Think about what you've written there calmly and you'll see I'm talking about an elliptical transfer alone instead of requiring an expensive drop down to a circular orbit which is not required and you only think is required if you are only thinking about circles. :)
The transfer you are talking about is just the WRONG TOOL. It is for changing radius when the problem is changing angle. To use an analogy you are taking a knife to a gunfight and holding it by the wrong end because you are using it the wrong way
GRAVITY EXISTS!
Why do you think satellites eventually fall to earth? I suppose if you have ignore that it explains why you think things an overly simplistic approach is justified.
And you are the one calling me ignorant?
FFS - learn something about what you are writing about before pretending you know as much as you should have learnt at high school it you'd taken physics or any decent mathematics subjects.