Showing posts with label geostationary orbit. Show all posts
Showing posts with label geostationary orbit. Show all posts

Sunday, August 11, 2019

An archaeological perspective on orbital stratigraphy

One of the things I've been thinking about for a while is the the structure of the archaeological record of Earth orbit - all the spacecraft that have been launched over the last 60 years, and their decay products, fragments and molecules of Earth-manufactured materials. Something people ask me occasionally is how you can do archaeology when there is no stratigraphy. In terrestrial archaeology, everything eventually falls to the ground and becomes buried as winds, water and human activities erode higher places and move the sediment to lower places. Generally, the deeper you dig, the older the remains that you find.

This isn't how it works in Earth orbit. Everything's falling, for sure - but a large proportion of stuff never reaches the ground. It's all up there, the new mixed up with the old, the functioning with the defunct, the living with the dead. It's not a mirror of stratigraphy on Earth. The lower something is says nothing about how recent it is.

With one exception - everything in geostationary orbit is younger than 1963, when Syncom 3 became the first satellite to successfully reach this critical orbit, the importance of which for telecommunications had been predicted since the early 20th century. This is just seven years after the first satellite though - not very long. And there's only about 40 satellites left in orbit which date from this period.

Multigravity environments

It's more useful not to think of Earth as the standard, but as a special case in a solar system comprising many different levels of gravity and many different ways of experiencing it. For example, when we talk of microgravity in Earth orbit, it's not really that there is no gravity. The Earth is still there, pulling everything towards it as usual. It's the acceleration of falling towards it that creates the sensation of microgravity. You can experience the same thing in a droptower ride at an amusement part or the zero-gravity 'Vomit Comet'. You don't even have to leave Earth to have different gravity experiences!

The nature of the archaeological record varies according to the gravity you're in. In full Earth gravity, a powerful attractor, things fall. In Earth orbit, things float but can get pulled back to Earth by atmospheric drag. On the Moon, things fall, but more slowly, and less energy is needed to throw them up into orbit. At the five Lagrange points in the Earth-Moon-Sun system, things bounce around. (Indeed, just recently, they have been shown to be massive dust traps).

Lagrange points in the Earth-Moon-Sun system. Image credit: NASA


I prefer to conceptualise the way artefacts respond to variable gravity environments as a dynamical system. This is a visual, mathematical way of representing how objects move over time when certain boundary conditions are set. Objects are the recipients of energy through various sources, and gravity determines how much energy the objects need to move. The dynamical system is a map of places where objects end up as they lose energy - the process of entropy. Effectively, such a map is also an archaeological plan of a site or the surface of an excavation unit. (Now I wonder if we should be regarding our plans as frozen moments in a dynamical system, just one that is generally moving a lot more slowly than orbit. So the critical difference between the two regimes is not speed, but time).

These places are points of stable or unstable equilibrium. When an object falls to the ground, it's in a stable equilibrium place of low energy. To get off the ground, energy has to be added. The energy might come from someone kicking it, or a stream of water which moves it on. The Lagrange points include both stable (L4 and L5) and unstable equilibria (L1, L2 and L3). Unstable equilibrium is like balancing an egg on its pointy end: you can do it, but it's going to fall over pretty quickly. (Also, it helps if the egg is hard-boiled). Using this as a framework, Earth and Earth orbit are not completely different places with different rules, but places within the same system with different amounts of energy.

It also helps to visualise this as an Einsteinian gravity well. The bottoms of the wells are points of low energy and stable equilibrium.

A 2-D slice of a gravitational force vector field (left) is interchangeable with a 3-D gravity well (right), with the z-axis showing energy (potential). Image courtesy of Invent2HelpAll

How junk disperses, or a taphonomy of orbit

In fact, the stratigraphy of space junk does include a terrestrial component. The lowest point of energy in the orbital dynamical system is the surface of Earth: an orbit of zero apogee and perigee. The atmosphere is a barrier or boundary between different gravity regimes, as space objects can bounce off its upper surface, and those that get pulled into it tend to incinerate. However, some spacecraft parts are made of materials like stainless steel and titanium alloys, which have high melting temperatures. Other parts may have carbon-carbon insulation which provides some protection from temperature extremes. Sometimes these components scream at high speed into the atmosphere, with their flesh burning, and fall with a smoking thud to the surface. The so-called 'space balls', titanium pressure vessels, are one of the most common spacecraft parts to survive re-entry. These spheres are the best gravity travellers; they get to come back.

Of course little of the spacecraft is likely to remain in orbit after the main body has re-entered - perhaps some molecules or broken-off bits. When we find the space balls or other Earthbound space junk, it's most likely that this is all that remains of the spacecraft. They've fallen to the point of lowest energy. This includes the spacecraft graveyard at the bottom of the ocean. Earth orbit is bookended by graveyards, if you take into account the graveyard orbit a few hundred kilometres above the geostationary ring. This is where old GEO satellites go to rest in their undead way, as they can still drift down and across the orbits of living satellites.

In general the the structure of space junk is not vertical layers as we're accustomed to in archaeology. Instead, spacecraft decay fragments have an elliptical or cloud geometry. When a spacecraft is whole, all its components are on the one orbital trajectory. Now imagine a solar panel detaching from the main body. Initially, its speed and orbit will be pretty much the same as the main body. But as time passes, the orbits will diverge. If the panel is tracked by one of the Earth-based telescopes, then we will have all the data about it's orbit into the past and will be able to trace it back to the original spacecraft - as long as we keep tracking it.

If a spacecraft explodes, the debris initially forms a cloud around it. The cloud travels together for a little while and then the individual pieces, all with their own weight, size, shape and velocities, start to disperse. If you look at the orbital tracks of Fengyun 1C, the Chinese satellite which was the target of a test missile shot in 2007, the debris rapidly moves apart and starts to spread out as you see here:

Image result for fengyun 1c
Fengyun 1C debris evolution. Image by Karl Tate @space.com

Position in orbit is described using a set of six equations devised by Johannes Kepler. Usually what people use, however, is Two-Line Elements - a bit like Eastings and Northings. The position is simplified into two strings of numbers. But because of the non-linear unpredictability of orbits, the reliability of the TLEs diminishes pretty fast. After 30 days you can't be sure that the TLE will accurately predict where something is. What this means in practice is that objects have to be continually watched or tracked to know where they are. This is called persistent observation and it's not generally something archaeologists worry about on Earth. However, artefacts on the surface do move around, although very slowly. You can record a concentration of stone artefacts on the surface, but if you revisit the same site a year later, half of them might be missing. Some have worked their way underground; some are covered by vegetation; others have moved under the influence of wind, water, animal movement or land use and industrial activities. Ten years into the future, there may be nothing to see. So perhaps I should apply the principle of persistent observation to terrestrial archaeology after all...

Objects in space are, of course, moving at incredibly high speeds - an average of 7-8 km per second. It's not that objects within archaeological deposits don't move; soils can act as liquids over a long time period, with a gravity-driven convection that gradually makes artefacts rise higher in the profile. Sometimes objects rise to the surface like a fish and get stranded there. Others, like stone tools with narrow sharp edges, slip back in for re-circulation. This is something archaeologists are very interested in as it says something about the integrity of the site and the relationship between objects. We're looking to that relationship to try and work out the human behavioural correlates, so we need to understand how the relationships decay over time due to natural or cultural factors, such as water movement or scavenger activity.

It's the relationship that matters

Both inside Earth and in orbit, the way the relationships between objects within a space evolves over time is critical to working out the human behavioural component. Looking at how the space debris environment evolves, it seems that after a certain amount of time it would be impossible to reconstruct the orbital path and work out what spacecraft a piece of junk came from, if you did not already have tracking records. Let's imagine the scenario of a future human archaeologist after the records have vanished (we can't assume they will survive in their current form) or even an alien archaeologist looking at space debris to get a handle on Earth culture. They will initially use materials and style to identify which space objects belong in the same time frame or to the same culture. They'll also have to work out what differences are due to style, and which to function.

Effectively, orbital archaeologists of the future will be 'recapitulating' a period of terrestrial archaeology before there was absolute dating, when similarities in style were used to posit chronological and social relationships. This period of investigation is known as culture history, and it worked on a number of premises. The first was the definition of culture, which as V. Gordon Childe phrased it, was a consistently occurring suite of artefact types, features and structures that you could attribute to an ethnic group. The second was the assumption that things change over time, coming in and out of fashion. Graphs of the frequency of occurrence of different artefacts types or styles resembled battleship curves, as they were known. Something starts out at a low frequency, then its numbers increase as it becomes popular. Soon the next big thing starts to supersede it and the frequency declines until no-one makes or uses the object any more. This is pretty much what happens in the fashion industry. Using changing frequencies to date an object is called seriation.

Because atmospheric drag pulls objects out of Low Earth Orbit all the time, things that survive there will be those with the greatest numbers, eg rocket bodies. This makes it a matter of sampling. Future archaeologists may not find the rare satellites as easily as the common ones. It's like the famous section in Kent G. Flannery's The Early Mesoamerican Village, a classic of the 1960s-1970s movement known as the New Archeology. A Real Mesoamerican Archaeologist laughs about another's failure to find the city of Teotihuacan using a particular sampling strategy. The Skeptical Graduate Student explains that this is not the purpose of a sampling strategy - and that the sample should produce results in proportion to what exists in the entire population of artefacts.

In another post I'll consider whether we can apply absolute dating techniques to space junk in orbit.


Topological stratigraphy

Terrestrial stratigraphy is locally linear and Euclidean, but orbits are non-linear and non-Euclidean. At larger scales, space is better described as the topological object called a manifold. Stratigraphy might simply be the wrong concept to describe the structure of orbiting objects. What kind of word would we use instead? Perhaps gravigraphy - written in gravity? Or orbitography, which is 'the determination and positioning of satellite orbits by a form of geodesy'?

Visualisations of space junk show Earth surrounded by white dots, like a cloud of silent bees. If you took Earth out of the middle, you would have a donut shape or torus where geostationary satellites are concentrated, and perhaps a series of intersecting tori for low to medium Earth orbit satellites. This is in stark contrast to terrestrial stratigraphy, which is conceptualised in a box-shape (even though Earth is spherical). Objects in this gravitationally-constrained tori move on elliptical paths inside the shape.

Let's put Earth back in. If we sliced a wedge vertically through through this cloud or swam, and froze the objects within it, what would we see? At the outer edge, the graveyard orbit, there'd be a thin smattering of defunct satellites. They are all dead. Below it, in the GEO range, there is thick ring of living and dead satellites. The 'type fossil' of this layer is the winged bird.

Then there is a sparse background scatter of satellites and junk until we hit the navigation satellites in the Medium Earth Orbit range. The US GPS network orbit at around 20, 000 km.

In LEO, we get the highest density of rocket bodies as well as satellites. There is a more diverse size range, from ENVISAT, the International Space Station, to cubesats and nanosats. There is the sparsest smattering of organic material.

There's a dead zone from LEO to the height of the tallest building or structure on Earth. Birds and aeroplanes fly at different altitudes, but they don't stay there or live there. There are gases, clouds, dusts.

On the surface of Earth, the ancient is mixed up with the modern. I suppose it is more like orbit than we might think, the living and the dead jostling side by side. Organic material is dense. Movement is slow. The deeper you go under the surface, the older things become. In this subterranean sphere, everything human is dead.

In all of these layers, the past and the present are mixed up to different degrees. The closer to the present you get, the higher and deeper human culture goes. Mines and building foundations cut into the dead deep past and overlay it with modern material. This is the variable borderland between the Pleistocene, Holocene and Anthropocene, a diachronous boundary that archaeologist Matt Edgeworth and his co-authors (2015) have discussed in an insightful paper (see below).

What is a place in orbit?

I'm relatedly curious about the concepts of setting or site in the orbital environment. Here, a 'place' is really a set of equations that defines the way an object moves - not just now but in the past and into the future. Place is a prediction, effectively. Place is movement, not stasis.

Could an orbital pathway, in and of itself, have heritage significance? Could it be 'preserved', and what would be the relationship between a culturally significant trajectory and the equations that define it? Could those equations, in and of themselves, also be considered culturally or archaeologically significant?

Perhaps in the future, there will be markers along the orbits of significant spacecraft that are not longer there, alerting anyone/thing who approaches that they are at a heritage orbit. Perhaps certain orbits - like Vanguard 1's - could be registered as significant so that nobody can launch something into the same orbit. An orbit has economic significance - so why not heritage significance too?

I think I have a lot further to go in this line of thinking. But it's a start anyway.


References

Matt Edgeworth, Dan deB Richter, Colin Waters, Peter Haff, Cath Neal, and Simon James Price 2015 Diachronous beginnings of the Anthropocene: the lower bounding surface of anthropogenic deposits.  The Anthropocene Review 2(1):33-58

Flannery, Kent G. (ed) 1976 The Early Mesoamerican Village. Academic Press


Saturday, April 25, 2015

When geostationary orbit became real: the cultural significance of Syncom 3

Syncom 3 was the first true geostationary (GEO) communications satellite, launched in 1963, nearly two decades after Arthur C. Clarke predicted the potential of GEO for telecommunications. Prior to the Syncom series, communication satellites were located in Low Earth Orbit (LEO) where they required massive terrestrial infrastructure. Syncom 3 was aimed at providing live television coverage of the 1964 Olympic Games in Tokyo, as well as carrying telephone transmissions. But its uses were not confined to the civil sphere. Syncom 3 and its geosynchronous sister Syncom 2 were the primary communications link between South East Asia and the western Pacific in the Vietnam War.

Syncom 3
Image courtesy of NASA
Only six years after the first satellite, Syncom already shows how satellite design has moved past the early templates of the baby moon (Sputnik and Vanguard) and the rocket (Explorer 1). The Syncom series were the first spin-stabilised satellites. The basic design is still in use, for example, in the Aussat and Optus B series.

Syncom 3 is the ancestor of the satellites that provide telecommunication services today. Technologically, Syncom 3’s design and mission helped shape the world of the second millennium where nearly everyone is within reach of almost every point on the globe, and transnational entities flicker and spark into existence between hardware on Earth and in orbit.

Syncom 3 was a major step in the process of globalisation that has been developing since the 1400s when navigation connected previously separate old and new worlds. For some, globalisation has meant new possibilities and opportunities; for others, it has meant the erosion of identity in contexts where colonial exploitation has already exacted a high cost.


Note: This is an excerpt from Gorman, A.C. 2005 The Archaeology of Orbital Space.
In Australian Space Science Conference 2005; pages: [338-357]. Melbourne: RMIT University.


References
Clarke, A. C., 1945 Extraterrestrial relays: can rocket stations give worldwide radio coverage? Wireless World, October, 1945, pp 305-308


Wednesday, June 18, 2014

Archaeology and Heritage of the Human Movement into Space

A new book on space archaeology is about to be released (August): Archaeology and Heritage of the Human Movement into Space, edited by Beth Laura O'Leary and P.J. Capelotti. It's based around papers from a session at the Society for American Archaeology last year.

My offering is about the kinds of data we can access about orbital objects and their cultural meanings. A key part of my argument is based around a brilliant photograph taken by Dr Marco Langbroek, a Palaeolithic archaeologist and astrographer, of a section of geostationary orbit. I look at what the spatial relationship between the satellites says about geopolitics, the spectrum landscape between Earth and space, and even go a bit of Deleuze and Guattari (this surprised me as much as I expect it surprises you).

Here's a taster:
Spectrum is both a driver of satellite telecommunications technology and an invisible ‘soup’ in which the spacecraft swim. This makes it very different from sensory landscapes of human interaction, composed of visible light wavelengths, sound, and the molecular interactions of smell and touch. It is truly non-human and robotic; our interaction with it can only be mediated by antennas and signal processors.
And there's much more where that came from.

There are many other fascinating chapters, and we're very excited about the book, which captures the state of the discipline 11 years after the 5th World Archaeological Congress in 2003.


Wednesday, October 27, 2010

A space debris-tracking satellite

 WASHINGTON — NASA’s Marshall Space Flight Center is gathering information for the possible development of a demonstration satellite to track pieces of orbital debris that are too small to be seen by current systems but still pose a threat to operating spacecraft. Spurred by the new U.S. National Space Policy that emphasizes tracking and mitigating orbital debris, Huntsville, Ala.-based Marshall may partner with industry and academia to field a low Earth orbiting satellite as soon as 2014, said Bruce Wiegmann, an engineer in Marshall’s Advanced Concepts Office (full story at http://spacenews.com/marshall-ponders-debris-tracking-demo-satellite/)

This is an interesting concept, as, in my opinion, there isn't enough of this going on at the moment.  Debris in GEO is not as well modeled as lower orbits because of the difficulties of tracking stuff that far away; but there are only a few satellites being used to obtain data on GEO (at least as I understand the situation).

This demo satellite is aimed at tracking debris from 1-10 cm in diameter, what's known as the medium-sized class.  The stuff above 10 cm is well tracked from Earth. The problem with the medium debris size class is that collision with a piece can cause a lot of damage to a functioning spacecraft, and even mission failure. And there's far more of it than the big stuff, so collision is far more likely.

I will have to keep an eye on this development to see if there are implications for space heritage.




Monday, May 10, 2010

Zombiesat joins the ranks of space junk

Zombiesat! What's Next for the Out-of-Control Galaxy 15 Satellite

By Clara Moskowitz
SPACE.com Senior Writer
posted: 04 May 2010

The Galaxy 15 commercial satellite that recently lost contact with the ground has joined the ranks of a boatload of other debris adrift in space. It's now termed a "zombiesat" by engineers who have a better sense of humor than you might have imagined. So what's next for this 4,171-pound (1,892-kg) zombiesat?

This defunct satellite will probably drift to one of two "gravity wells" that catch most out-of-control spacecraft, experts say. Galaxy 15 could threaten nearby satellites because its communications package is stuck on and it may start interfering with its neighbors by siphoning off their signals. It's the first time such an event has ever occurred, and it sent Orbital Sciences, the satellite's builder, on a dash to figure out how to stop the satellite-run-amok.

Galaxy 15, like many communications satellites, was circling Earth about 22,369 miles (36,000 km) high in what's called geosynchronous orbit, meaning that it orbited at the same speed the Earth rotates, so that it sat perched above the same part of Earth all the time. "There are two points in geosynchronous orbit called geopotential wells," explained Nicholas Johnson, chief scientist for Orbital Debris at NASA's Johnson Space Center in Houston. "These are perturbations in Earth's gravity field. Typically when satellites lose control they will drift toward the nearest geopotential well and just oscillate around it." The two spots, also called libration points, are located at longitudes of 105 degrees west and 75 degrees east. There are already between 150 and 200 objects oscillating around these points, Johnson said.

Still a large place
In that sense, the new zombiesat doesn't significantly increase the space debris problem or pose a serious risk of colliding with an operational satellite.

"Space is still a very large place," Johnson told SPACE.com. "There are a lot of objects that are drifting back and forth. Galaxy 15 really just kind of joins a relatively large number of objects – it's not a significant new hazard from a global standpoint. But if your satellite happens to be near where Galaxy 15 is drifting then it's of more concern."  Eventually, everything in low-Earth orbit will eventually fall back down toward Earth because of atmospheric drag. The small amount of atmospheric particles in space create friction with spacecraft, causing their orbits to decay. The time it takes for an object's orbit to decay depends on its altitude.

For example, the International Space Station orbits at about 250 miles (400 kilometers) above Earth, while the Hubble Space Telescope circles much higher, at 353 miles (569 km).  "When things fall off the International Space Station, they typically fall back within a couple months, but where Hubble is, it typically takes several years to fall back to Earth," Johnson said. "At 800 km you're talking many decades or even hundreds of years."

To prevent the buildup of dead spacecraft in heavily trafficked areas of geosynchronous orbit, guidelines recommend that when a satellite reaches the end of its life it is boosted to a higher orbit out of the way. This "graveyard orbit" is about 186 miles (300 km) above where most satellites orbit. "The whole idea is to get to an altitude so they don't drift back into the operational region for a very, very long time – over 100 years," Johnson said.

It's actually easier to boost a spacecraft up just this much higher than to maneuver a craft down to where it would immediately fall back to Earth and burn up in the atmosphere, he said.

Getting rid of space junk
To actually go and collect defunct spacecraft to remove the collision risk altogether is currently beyond our ability.  "Unfortunately we haven't found a concept which appears to be both technically feasible and affordable," Johnson said. The best way to remove spent rocket stages and other large objects from orbit is to simply send up another spacecraft to rendezvous and dock with it and drag it back down to earth. This method would be extremely expensive and time-consuming, and isn't viable for the vast number of objects already in space. Some more exotic measures involving tethers and other props have been proposed, Johnson said, but aren't yet feasible.

For getting rid of very small pieces of space junk, there are two favorite ideas, he said. One involves shooting lasers at the objects to push them into lower-altitude orbits so they fall back down to Earth more quickly. "That has technical, economic, as well as policy issues," Johnson said. Another concept is to fly up a structure with a large area but low mass so that when particles strike the surface they will penetrate and lose some of their orbital energy, causing them to fall back to Earth more quickly. This option would also need many technical issues ironed out. "If it was easy we'd already be doing it," Johnson said of tackling the debris problem. "But it's prudent to be working the issue now before it becomes a serious impediment to space operations."


Friday, April 09, 2010

CubeSail - active orbital debris removal moves closer to reality

UK researchers have developed a device to drag space junk out of orbit.
By Jonathan Amos
Science correspondent, BBC News  
26th March 2010
 
They plan to launch a demonstration of their "CubeSail" next year. It is a small satellite cube that deploys a thin, 25-sq-m plastic sheet.  Residual air molecules still present in the spacecraft's low-Earth orbit will catch the sheet and pull the object out of the sky much faster than is normal. 

The Surrey Space Centre team says the concept could be fitted to larger satellites and even rocket stages.  The group also envisages that a mature system would even be sent to rendezvous and dock with redundant spacecraft to clean them from orbit. "Our system is simple and very low cost; but we need to demonstrate that it can be done," said Dr Vaios Lappas, lead researcher on the project and senior lecturer in space vehicle control. "It would help make space a sustainable business. We want to be able to keep on launching satellites to provide new services; but unless we do something, the amount of junk up there is going to grow exponentially." 

Simplicity of approach
It is thought more than 5,500 tonnes of junk now clutters the region of space just a few hundred km above our heads. Last year, two satellites even collided, showering their orbit with tiny fragments that now pose additional risk to operational spacecraft.

International agencies have agreed that retired hardware - old satellites or spent rocket stages - should be removed from space within 25 years of the end of service. Using large deployable surfaces to increase the drag on these objects so they fall to Earth rapidly is one possible solution to the space litter problem. CubeSail, unveiled on Friday, is a 3kg (6.6lb), 10cm x 10cm x 30cm (4in x 4in x 12in) nanosatellite. It incorporates within its tiny frame a polymer sheet that is folded for launch to be unfurled once in space. The simple deployment mechanism features four metal strips that are wound under tension and will snap into a straight line when let go, pulling the sheet flat in the process. 

The team hopes to launch its demonstrator at the end of next year, riding piggy-back on another mission or as part of a cluster of small research satellites that are sometimes lofted en mass atop a single rocket. 

Force of sunlight
The nanosat will then circle the Earth, going from pole to pole at an altitude of about 700km (435 miles), testing its systems and assessing the drag principle. If successful, CubeSail could become a regular add-on system to satellites and rocket stages, opening up a new space business akin to the daily refuse services here on Earth. 

"We would be looking to put it on our own satellites and to put it on other people's spacecraft as well," said Sir Martin Sweeting, the chairman of SSTL, the world-leading small-satellite manufacturer, which is supporting the research.  "We want this to be a standard, essential bolt-on item for a spacecraft; and that's why it's very important to make it small, because if it's too big it will interfere with the rest of the spacecraft," he told BBC News.

The researchers hope to develop the project as a propulsion system as well. The pressure of sunlight falling on such a large structure would also move it. The force is tiny but continuous. This "solar sailing" technique has long been touted as a means of moving spacecraft around the Solar System, or even just helping conventional satellites to maintain their orbits more efficiently. Indeed, some of the large geostationary satellites, for example, already use solar-sail flaps to maintain their attitude without firing their thrusters. This saves valuable chemical propellant and extends mission lifetime. 

Delicate control
CubeSail will endeavour to demonstrate this "propellantless propulsion" by trying to shift the path it takes across the surface of the Earth by just a few degrees over the course of a year. To do this though, the nanosatellite will have to carefully control the angle of the sail with respect to the Sun, just as an ocean vessel has to play with its sails to catch the wind.
Sail deployed in lab (SSC)

"We're going to control our sail with a very novel geometric technique; we're not going to use any thrusters," explained Dr Lappas. "We have developed a tilting mechanism that uses very tiny motors. It's able to move in two directions. This enables you to change the centre of mass of the sail. We're also going to be using small magnets to control the sail because they will interact with the Earth's magnetic field."  Once its mission is complete, CubeSail will be instructed to take itself out of orbit.

The project is a private venture within the Surrey Space Centre, which is based at the University of Surrey, Guildford.  CubeSail has been funded by Europe's largest space company, EADS Astrium, which is one of the world's biggest manufacturers of satellites. It also produces Europe's heavy-lift rocket, the Ariane 5, which launches about half of the world's commercial satellite platforms. The entire cost of the project is expected to be no more than £1m ($1.5m). 

Other groups around the world are expected to launch solar sail demonstrators soon. The US space agency has been working on a project with The Planetary Society, a long-time proponent of the technology. The Japanese, too, have work in progress. And even Astrium is sponsoring other space junk mitigation strategies within its own division. 



Sunday, November 02, 2008

Graveyard orbit on the World Heritage List

Don't get too excited, I'm just thinking about it.

The graveyard orbit is located above the Geostationary ring, where most of our telecommunications satellites operate. Many of them are left with sufficient fuel at the end of their mission life to boost them into this orbit, where they are out of the way and not contributing to the debris problems in GEO.

It's not that they are now simply inert - I have seen discussions of how material in the graveyard orbit can impact on spacecraft in GEO - and let's not forget that we're talking about many-body problems here with all the instabilities of non-linear systems, so they may not always just circle up there serenely - but to all intents and purposes nothin' is going on in the graveyard orbit. It's not premium space, no-one wants it at the moment for anything except as a junkyard.

So if we were going to propose anything for world heritage listing in space, this may be a good choice: uncontroversial in terms of competition for space resources, without the nationalist interests of places like the Moon, and easy to enforce!

The WHL cannot be applied to space at the present time, but I'm working on this with the help of my graduate student Nigel and space lawyer Anthony Wicht.

The question of its significance is another I'll have to investigate.


Thursday, February 07, 2008

Arthur C. Clarke and the lingua franca of the future

Who rules the moon controls the earth, it is true, but only to some extent - as Arthur C. Clarke pointed out once, control of GEO is even more important as telecommunications determine which culture achieves hegemony through linguistic dominance.

Hegemony is such a good word and reminds me that I am thinking of calling my WAC-6 paper "Prolegomena to space archaeology" because prolegomenon is an excellent word too. I think of them in the same breath as both are Ancient Greek words that have survived in English two and bit millennia later. But would such a title sound too arcane?


Thursday, July 12, 2007

The first seven years in orbit

The ICOMOS Australia conference is on in Cairns next week. John Campbell and I are convening a session on space heritage, and we're very excited, because Beth O'Leary from New Mexico State University is visiting Australia for the first time. Beth has been researching Tranquility Base and will deliver one of the keynote talks.

As per bloody usual, I'm writing my paper at the last minute (why, oh why, do I always do this?). I'm looking at the material record in orbit from 1957, the launch of Sputnik 1 into Low Earth Orbit, until 1963, when Syncom 1 is launched into geosynchronous orbit. Only seven years to get from LEO to GEO, and then another seven years until people land on the Moon. Pretty astonishing.

Looking at the figures has raised some interesting points. I expected to see a more or less equal distribution of USA/USSR satellites still up there. But the satellites remaining in orbit from the first seven years are almost entirely US, the main exception being Canada's Alouette 1. What happened to the Russian satellites?

One reason they are underrepresented is because during this period the USSR was focussing on the Moon, so quite a few have ended up in lunar orbit or cislunar space. (This makes me realise I don't know much about how lunar orbits work, in the absence of aerodynamic drag. Must find out). (And isn't cislunar a fabulous word?). Numerous other missions were crewed, and thus returned to Earth.

Another explanation may be that USSR satellites were injected into lower orbits than USA ones and have decayed at a greater rate. I won't have time to pursue this before the conference unfortunately.

I am going to imagine a scenario where all we have is the orbital material to work out how humans got into space. What will this first seven years tell us, and how might it differ from the documentary record?

I'm also going to take a closer look at the fascinating West Ford project ....



Thursday, July 29, 2004

Syncom 3

Syncom 3 was the first satellite to be launched into geostationary orbit, after Arthur C. Clarke had predicted the use of GEO for telecommunications in a 1945 article for Wireless magazine. I must do some more research about its possible heritage significance.