ESA Satellite Recovers: Total Loss To Geostationary 47
Slimbob writes "About 2 years ago an Ariane 5 rocket malfunctioned and left a very expensive Artemis satellite in an unusable orbit. Well, over the course of 18 months, the European Space Agency actually managed to push the satellite into a usable orbit using measly 15mN ion thrusters! They managed the feat by reprogramming about 20% of the original control software and uplinking the patches to the satellite! See the ESA press release . Achievements include the first first major reprogramming of a telecommunications satellite, the first orbital transfer to geostationary orbit using ion propulsion, and the longest ever operational drift orbit."
Fuel (Score:3, Interesting)
Re:Fuel (Score:5, Informative)
The article makes a distinction between the Xenon ion thrusters and "chemical propellant". The last orbital adjustments were made with "small chemical propellant thrusters, activated for the first time since launch".
It looks like the 10 years number does not refer to the Xenon ion thrusters.
Re:Fuel (Score:2, Interesting)
Re:Fuel (Score:3, Informative)
A Google search for "ion thrusters" returned a wealth of information, much of it suitable for an introduction. An excellent one is here [twtas.com].
These devices are not new -- they have been in use for years.
Re:Fuel (Score:2, Informative)
Deep Space 1 was more impressive (Score:2)
Re:Fuel (Score:2)
Re:Fuel (Score:4, Interesting)
Since the operational drift is so much longer then what was originaly antisipated, I would be that they are consuming much less propellent then originaly expected, so they are able to get "10 years" out of what is left.
GStar 3 or 4, put up by GTE in the late 80s, had a simmilar fate. It was lobbed into a bad orbit, written off (paid for), and then slowly (very slowly) moved into a "usable" orbit. The satellite had less propellent avaiable to it, so it was allowed to drift up and down, and side to side.
GTE sold cheap time on the satellite since you could only get 5 to 20 minutes at a time without re-aiming your uplink antenna. A friend of mine wrote the software (in basic) that people used to aim thier uplinks antennas. However, since the satellite was paid for already, any money coming in was gravy at that point.
I stand in awe... (Score:1)
This isn't the first innovative satellite recovery (Score:5, Informative)
Reference: Flug-Revue [rotor.com]
Re:This isn't the first innovative satellite recov (Score:2)
"15mN ion thrusters" (Score:4, Funny)
See honey, size doesn't matter!
Re:"15mN ion thrusters" (Score:5, Funny)
Re:"15mN ion thrusters" (Score:1)
Re:"15mN ion thrusters" (Score:2)
Don't understand their error rate calculations (Score:1)
I don't get this bit. If the bit error rate was measured at 1 in 109, surely that means that there should be approximately one bit received erroneously per 109 bits? How do they get a billion? Or is that in conjunction with an error correcting code?
Re:Don't understand their error rate calculations (Score:1)
Probably attained with error-correction, too.
Re:Don't understand their error rate calculations (Score:5, Informative)
Re:Don't understand their error rate calculations (Score:1)
Re:Don't understand their error rate calculations (Score:1)
Cool Hack (Score:3, Insightful)
Great (Score:2)
Re:Great (Score:1)
Re:Great (Score:2)
Basically Kepler made postulates (planets follow elliptical orbits with the Sun at one of the foci; planets sweep out equal areas in equal time; planet orbital period relationship to the orbital radius) that fit the data pretty well. Newton mathematically derived these from first principles and added corrections (e.g., the planets don't orbit the Sun, the Sun and planets orbit each other) that fit observations even better. Newton also starting working on the higher order correction terms to describe planetary motion when other bodies are present, which is the three-body (and higher!) problem (the three-body problem, by nature of not being integrable, has occupied the minds of some of the biggest names in mathematics ever since). I believe that above statement is true, that how satellite/spacecraft orbits are calcuated is essentially the same method that Newton was using when working on planetary orbit corrections.
Expect more ions in the future (Score:5, Interesting)
More to the point... (Score:2)
Wow (Score:4, Funny)
Re:Wow (Score:1)
Ah, that's what they *want* you to think... (Score:2)
Damn. It's obvious that Planetary's [earthlink.net] efforts on behalf of mankind have been negated yet again...
On patching satellites (Score:3, Interesting)
Seems like somebody probably thought it through for the cost of one of these programs.
Re:On patching satellites (Score:3, Interesting)
I would figure they probably use a more elaborate system...but it's probably the same in practice...of course, they have simulators/emulators on the ground that can accurately recreate the satelite's internal components...so, there should be no bugs in the system when the patches are sent...
The only thing they'ld need to worry about is noise on the uplink (corrupted files) and possible hardware failure...corrupted files could be tested for prior to patching, and hardware problems can be fixed by having backup systems...
Re:On patching satellites (Score:1)
Fuel: Why not... (Score:2)
include a docking port, so you can send a 'cargo satellite' after it to refuel your $10^8 satellite?
This would be expensive [1], but a lot less so than writing off a satellite that ends up in the wrong orbit. Also, you could keep your satellite operational far longer than usual: communications satellites IIRC are written off when they run out of fuel, rather than because of mechanical/electrical failures.
1: or would it? You'd have to launch it, but you're launching just a load of fuel with some maneuvering motors attached to it.
Re:Fuel: Why not... (Score:3, Insightful)
-T
Re:Fuel: Why not... (Score:3, Insightful)
No, your energy is already up there. AFAI understand, you still need to bring something that can be ionized, then accellerated to provide the actual thrust. Advantage of the ion drive is that the exhaust speed can be higher than with a chemical rocket, so you need less fuel to produce the same thrust.
Re:Fuel: Why not... (Score:2)
Should have confirmed here first. [northwestern.edu]
Still, though, signifigantly less fuel.
-T
Re:Fuel: Why not... (Score:1)
The satellites electronics go obsolete before they run out of fuel. In general it is better for a company / country to boost a whole new sat with higher bandwidth, better resolution, more accuracy (depending on the sats design goal) and move the old one into a graveyard orbit.
The exceptions to this tend to be science sats which are hard to get funding for and / or in weird orbits. In those cases it is a choice between doing ground side changes to prolong the sats functional life or having no sat at all.
This instance was a unusual one becuase it was a brand new com sat that failed to achieve proper orbit; not an end of life sat running out of station keeping fuel. It isn't cost effective to add expensive refueling capability (and pay for the launch of refueling 'cargo satellites') to save the rare satellite that ends up in a wrong orbit that doesn't send it back into atmosphere and whose payload is fully functional. On a cost basis it is better to just get the insurance payout and build another sat.
Awe (Score:1)
Are there any means of going back to a safe version of the firmware, or are there means of automatically rebooting the on-board computer?
virve
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Been done before (Score:2)