• Satterlites and reception

    From Brian Gaff (Sofa)@21:1/5 to All on Thu Apr 14 10:03:56 2022
    Seems to me that the actual signal levels that are arriving at your lnb
    must be really small, and of course dependent on how the aerials are aimed
    on the sat itself, ie footprint. Also one supposes the closer to the horizon
    it is for aiming the dish, the more atmosphere it needs to travel through to get to you. Ignoring for a second the that close to the horizon will mean
    you need a higher dish to avoid things on the ground, , eventually these
    Sats must go faulty. What on earth do they do with them then, to avoid collisions. There must be loads of old ones up there by now. Do they save a
    bit of rocket fuel to boost them well away? If they do and the fault is in
    the link, they are presumably stuffed and have to let it wander about for
    ever.
    Brian

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  • From Robin@21:1/5 to All on Thu Apr 14 10:45:52 2022
    Yes, these days there are international standards for end-of-life
    satellites. The Astra ones hold enough fuel to move them to a parking
    orbit a bit higher than the geostationary ones.

    On 14/04/2022 10:03, Brian Gaff (Sofa) wrote:
    Seems to me that the actual signal levels that are arriving at your lnb
    must be really small, and of course dependent on how the aerials are aimed
    on the sat itself, ie footprint. Also one supposes the closer to the horizon it is for aiming the dish, the more atmosphere it needs to travel through to get to you. Ignoring for a second the that close to the horizon will mean
    you need a higher dish to avoid things on the ground, , eventually these
    Sats must go faulty. What on earth do they do with them then, to avoid collisions. There must be loads of old ones up there by now. Do they save a bit of rocket fuel to boost them well away? If they do and the fault is in the link, they are presumably stuffed and have to let it wander about for ever.
    Brian



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  • From Roderick Stewart@21:1/5 to briang1@blueyonder.co.uk on Thu Apr 14 10:28:17 2022
    On Thu, 14 Apr 2022 10:03:56 +0100, "Brian Gaff \(Sofa\)" <briang1@blueyonder.co.uk> wrote:

    eventually these
    Sats must go faulty. What on earth do they do with them then, to avoid >collisions.

    Nothing, as far as I know. Space is just a lot more, well, spacious
    than it's easy to imagine. Theoretically a point on the Clarke orbit
    must be just that, a point, but in reality the tolerance is probably a
    few tens of miles, and the satellites are only a few feet across.

    Rod.

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  • From David Woolley@21:1/5 to All on Thu Apr 14 10:43:43 2022
    On 14/04/2022 10:03, Brian Gaff (Sofa) wrote:
    Do they save a
    bit of rocket fuel to boost them well away?

    Yes. See <https://en.wikipedia.org/wiki/Graveyard_orbit>

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  • From R. Mark Clayton@21:1/5 to Roderick Stewart on Thu Apr 14 08:16:08 2022
    On Thursday, 14 April 2022 at 10:28:21 UTC+1, Roderick Stewart wrote:
    On Thu, 14 Apr 2022 10:03:56 +0100, "Brian Gaff \(Sofa\)" <bri...@blueyonder.co.uk> wrote:

    eventually these
    Sats must go faulty. What on earth do they do with them then, to avoid >collisions.
    Nothing, as far as I know. Space is just a lot more, well, spacious
    than it's easy to imagine. Theoretically a point on the Clarke orbit
    must be just that, a point, but in reality the tolerance is probably a
    few tens of miles, and the satellites are only a few feet across.

    Rod.

    They normally de-orbit geostationary ones to a different orbit, although normal decay will normally see them move out of the ecliptic, where live ones are maintained.

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  • From David Woolley@21:1/5 to R. Mark Clayton on Thu Apr 14 18:25:37 2022
    On 14/04/2022 16:16, R. Mark Clayton wrote:
    move out of the ecliptic, where live ones are maintained.

    Surely not the ecliptic. I think most satellite dishes have a beam
    width a lot less than 46 degrees, and I haven't noticed them nodding up
    and down during the course of the year. I'd expect them to be aligned
    relative to the earth's axis, not the earth's orbit, although I'd expect station keeping to be easier for the latter.

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  • From Brian Gaff (Sofa)@21:1/5 to David Woolley on Fri Apr 15 10:01:32 2022
    No they should not be out of the ecliptic, at least not by very mush as this would produce a now you see it now you don't for those near the edge of the footprint north or south.
    Brian

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    "David Woolley" <david@ex.djwhome.demon.invalid> wrote in message news:t39lei$fbm$1@dont-email.me...
    On 14/04/2022 16:16, R. Mark Clayton wrote:
    move out of the ecliptic, where live ones are maintained.

    Surely not the ecliptic. I think most satellite dishes have a beam width
    a lot less than 46 degrees, and I haven't noticed them nodding up and down during the course of the year. I'd expect them to be aligned relative to
    the earth's axis, not the earth's orbit, although I'd expect station
    keeping to be easier for the latter.

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  • From Brian Gaff (Sofa)@21:1/5 to All on Fri Apr 15 09:59:40 2022
    Nobody seems to have thought this through then. After all, one assumes orbit decay has to be only via solar wind at those altitudes. That would possibly make them very unstable, since the largest areas will be the solar sells,
    I'd imagine and station keeping by gyros can only continue while these are still working.
    Brian

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    "R. Mark Clayton" <notyalckram@gmail.com> wrote in message news:fb5194f3-2d5d-4a7f-9777-2bad0601e41bn@googlegroups.com...
    On Thursday, 14 April 2022 at 10:28:21 UTC+1, Roderick Stewart wrote:
    On Thu, 14 Apr 2022 10:03:56 +0100, "Brian Gaff \(Sofa\)"
    <bri...@blueyonder.co.uk> wrote:

    eventually these
    Sats must go faulty. What on earth do they do with them then, to avoid
    collisions.
    Nothing, as far as I know. Space is just a lot more, well, spacious
    than it's easy to imagine. Theoretically a point on the Clarke orbit
    must be just that, a point, but in reality the tolerance is probably a
    few tens of miles, and the satellites are only a few feet across.

    Rod.

    They normally de-orbit geostationary ones to a different orbit, although normal decay will normally see them move out of the ecliptic, where live
    ones are maintained.

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  • From Tweed@21:1/5 to briang1@blueyonder.co.uk on Fri Apr 15 09:06:03 2022
    Brian Gaff \(Sofa\) <briang1@blueyonder.co.uk> wrote:
    Nobody seems to have thought this through then. After all, one assumes orbit decay has to be only via solar wind at those altitudes. That would possibly make them very unstable, since the largest areas will be the solar sells,
    I'd imagine and station keeping by gyros can only continue while these are still working.
    Brian


    It’s all been thought through. All satellite launches have to have an end
    of life plan. Obviously, if control has been lost that plan might not be practical.

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  • From Brian Gaff (Sofa)@21:1/5 to David Woolley on Fri Apr 15 10:03:33 2022
    Hmm, lets hope its far enough away that if there is a destructive collision
    the debris does not enter the wanted orbit then.
    There was, a few years ago a number of spent top stages of Long March
    rockets exploding in space sending debris everywhere.
    Brian

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    "David Woolley" <david@ex.djwhome.demon.invalid> wrote in message news:t38qcf$mnk$1@dont-email.me...
    On 14/04/2022 10:03, Brian Gaff (Sofa) wrote:
    Do they save a
    bit of rocket fuel to boost them well away?

    Yes. See <https://en.wikipedia.org/wiki/Graveyard_orbit>

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  • From David Woolley@21:1/5 to All on Fri Apr 15 13:17:00 2022
    On 15/04/2022 10:01, Brian Gaff (Sofa) wrote:
    No they should not be out of the ecliptic, at least not by very mush as this would produce a now you see it now you don't for those near the edge of the footprint north or south.

    It's being on the ecliptic that causes that problem. In the extreme
    case, a satellite on the ecliptic would be well below the horizon for
    half of the year, at the poles. The plane through the equator is tilted
    at, about 23 degrees, to the ecliptic!

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  • From R. Mark Clayton@21:1/5 to David Woolley on Fri Apr 15 09:59:22 2022
    On Thursday, 14 April 2022 at 18:25:40 UTC+1, David Woolley wrote:
    On 14/04/2022 16:16, R. Mark Clayton wrote:
    move out of the ecliptic, where live ones are maintained.
    Surely not the ecliptic. I think most satellite dishes have a beam
    width a lot less than 46 degrees, and I haven't noticed them nodding up
    and down during the course of the year. I'd expect them to be aligned relative to the earth's axis, not the earth's orbit, although I'd expect station keeping to be easier for the latter.

    No not the ecliptic, I meant equatorial position. They will slowly drift once fuel for maintaining position is used up.

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  • From Brian Gaff (Sofa)@21:1/5 to All on Sun Apr 17 09:10:50 2022
    I wonder what the main causes of failure are? Obviously when being first positioned in the right place they use fuel, but often the stabilisation is then done by Gyros, unless every so often the solar wind has shifted them enough to need to use rockets to reposition. These days, one assumes this is mostly automated. I also often hear of some sats having spares already in orbit, but surely that would shorten their operational life, if the
    temperature cycling, aging of solar cells gyros etc, were taken into
    account.

    Brian

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    "Robin" <rbw@outlook.com> wrote in message news:4d680d01-54a2-ae7e-f270-c3c6f7535052@outlook.com...
    Yes, these days there are international standards for end-of-life
    satellites. The Astra ones hold enough fuel to move them to a parking
    orbit a bit higher than the geostationary ones.

    On 14/04/2022 10:03, Brian Gaff (Sofa) wrote:
    Seems to me that the actual signal levels that are arriving at your lnb
    must be really small, and of course dependent on how the aerials are
    aimed
    on the sat itself, ie footprint. Also one supposes the closer to the
    horizon
    it is for aiming the dish, the more atmosphere it needs to travel through
    to
    get to you. Ignoring for a second the that close to the horizon will mean
    you need a higher dish to avoid things on the ground, , eventually these
    Sats must go faulty. What on earth do they do with them then, to avoid
    collisions. There must be loads of old ones up there by now. Do they save
    a
    bit of rocket fuel to boost them well away? If they do and the fault is
    in
    the link, they are presumably stuffed and have to let it wander about for
    ever.
    Brian



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  • From Jim Lesurf@21:1/5 to rjfs@escapetime.myzen.co.uk on Sat Apr 16 10:15:35 2022
    In article <bqpf5hluei1nvtok2b754c0eurte6iip7v@4ax.com>, Roderick Stewart <rjfs@escapetime.myzen.co.uk> wrote:
    heoretically a point on the Clarke orbit must be just that, a point, but
    in reality the tolerance is probably a few tens of miles, and the
    satellites are only a few feet across.

    The Clarke (geostationary) orbit assumes that the only bodies in the
    'Universe' are the Earth and the satterlite. And that each is a 'point
    source'. Even so, the orbit has no inherent stability. i.e. any
    infinitesimal error doesn't tend to fall with time.

    In reality the Earth isn't a perfect 'point source', and the Moon, Planets, etc, all affect the movement, making it unstable.

    In practice I think they 'orbit' the sats about their nominal geostationary point, partly to get more sats using that point without all hitting one another. Partly because - as with JWST - this can counter some of the
    unwanted effects mentioned above. The trick is to keep these offsets small enough that they don't take the sat out of the effective field of view of ground dishes. No idea of the details, though, but I guess others here
    will.

    Jim

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  • From David Woolley@21:1/5 to All on Sun Apr 17 11:01:42 2022
    On 17/04/2022 09:10, Brian Gaff (Sofa) wrote:
    Obviously when being first
    positioned in the right place they use fuel, but often the stabilisation is then done by Gyros,

    Gyros are only used for attitude, not for position.

    As well as being used for position control, propellant is also used,
    from time to time, to dump the angular momentum accumulated in the gyros.

    The Wikipedia "graveyard orbit" article, I previously mentioned,
    suggests that the end of life burn uses about the equivalent of three
    months of normal propellant usage.

    Micrometeorite strikes and high energy sub-atomic particle strikes, can
    also cause sudden failures.

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  • From Jim Lesurf@21:1/5 to briang1@blueyonder.co.uk on Sun Apr 17 09:48:10 2022
    Gyros are fine for attitude/orientation. But you need reaction thrust to correct for the unavoidable drifts away from the required orbit whilst in
    use. That tends to mean 'consumables' (fuel) that eventually becomes
    depleted. The sat then has to be moved off to a 'graveyard' parking orbit
    to clear the way for a new sat. Which requires the last part of the consumables.

    FWIW the Russians have developed quite impressive 'plasma' electronic
    drives for space use that have a very high dV and fuel efficiency. NASA
    *has* been using these - but that now probably needs the past (very) tense
    now!

    Overall, though, a problem of course is all the 'junk' sat launches
    continue to leave in orbit somewhere. De-orbiting into the atmosphere is practical for some, but not all.

    Jim


    In article <t3gi2b$ec4$1@dont-email.me>, Brian Gaff \(Sofa\) <briang1@blueyonder.co.uk> wrote:
    I wonder what the main causes of failure are? Obviously when being first positioned in the right place they use fuel, but often the
    stabilisation is then done by Gyros, unless every so often the solar
    wind has shifted them enough to need to use rockets to reposition.
    These days, one assumes this is mostly automated. I also often hear of
    some sats having spares already in orbit, but surely that would shorten
    their operational life, if the temperature cycling, aging of solar
    cells gyros etc, were taken into account.

    Brian

    --
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  • From R. Mark Clayton@21:1/5 to Jim Lesurf on Mon Apr 18 04:06:25 2022
    On Monday, 18 April 2022 at 10:01:42 UTC+1, Jim Lesurf wrote:
    Gyros are fine for attitude/orientation. But you need reaction thrust to correct for the unavoidable drifts away from the required orbit whilst in use. That tends to mean 'consumables' (fuel) that eventually becomes depleted. The sat then has to be moved off to a 'graveyard' parking orbit
    to clear the way for a new sat. Which requires the last part of the consumables.

    FWIW the Russians have developed quite impressive 'plasma' electronic
    drives for space use that have a very high dV and fuel efficiency. NASA *has* been using these - but that now probably needs the past (very) tense now!

    Overall, though, a problem of course is all the 'junk' sat launches
    continue to leave in orbit somewhere. De-orbiting into the atmosphere is practical for some, but not all.

    Jim


    In article <t3gi2b$ec4$1...@dont-email.me>, Brian Gaff \(Sofa\) <bri...@blueyonder.co.uk> wrote:
    I wonder what the main causes of failure are? Obviously when being first positioned in the right place they use fuel, but often the
    stabilisation is then done by Gyros, unless every so often the solar
    wind has shifted them enough to need to use rockets to reposition.
    These days, one assumes this is mostly automated. I also often hear of some sats having spares already in orbit, but surely that would shorten their operational life, if the temperature cycling, aging of solar
    cells gyros etc, were taken into account.

    Brian

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    What usually happens is that new satellites are launched on a schedule, so that ones nearing the end of their operational life are replaced before they stop working. The old satellite then becomes a "spare" until it can no longer be used. With less
    need to keep them on station they don't burn up fuel. Sometimes satellites are slowly drifted around to a new position.

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  • From Jim Lesurf@21:1/5 to david@ex.djwhome.demon.invalid on Mon Apr 18 10:09:36 2022
    In article <t3goi7$nb7$1@dont-email.me>, David Woolley <david@ex.djwhome.demon.invalid> wrote:

    Micrometeorite strikes and high energy sub-atomic particle strikes, can
    also cause sudden failures.

    Perhaps also worth mentioning given current 'events' that sats may also be vulnerable to being hit by objects from an exploded object. Curious example
    of this risk cropped up a while ago when bits from a Russian object caused people on the ISS to take shelter just in case some impacted.

    Jim

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  • From Brian Gaff (Sofa)@21:1/5 to Jim Lesurf on Wed Apr 20 08:49:53 2022
    The Iss and its controllers do have radar looking many miles ahead so they
    can make course changes to avoid this sort of thing, but its the bits
    smaller than you can see that are the danger.
    For a while old Long March rocket bodies had a tendency to explode several years after they had been used, and of course this spreads tiny bits through several orbits, however, at 22,400 miles out, its still relatively clear of this hazard. That is not to say of course that malicious intent might cause problems at that altitude if a weapon was sent there. It has been
    demonstrated that a relatively small laser weapon can disable a satellite at quite long ranges. They do not have to blow it up, just hit something important.
    As we know several nations have misguidedly used fragmentation techniques
    to destroy various in orbit objects and thus create hazards for many other spacecraft. There is active research going on on cost effective ways to
    clear such particles, but however you do it you are bound to miss some.
    I remember when I could still see a bit seeing pictures of areas of the outside of the ISS where there were dings and dents and scrapes where tiny objects had hit it. Thus far no serious damage has been done but some
    handrails have had to be changed due to sharp edges of dings damaging the silicon on astranaughts gloves.
    They are normally covered in RTV compound for better grip.
    I think the only incident that was down to impact damage was an ammonia
    leak in a radiator, which had to be replaced.

    Brian

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    "Jim Lesurf" <noise@audiomisc.co.uk> wrote in message news:59dafe235bnoise@audiomisc.co.uk...
    In article <t3goi7$nb7$1@dont-email.me>, David Woolley <david@ex.djwhome.demon.invalid> wrote:

    Micrometeorite strikes and high energy sub-atomic particle strikes, can
    also cause sudden failures.

    Perhaps also worth mentioning given current 'events' that sats may also be vulnerable to being hit by objects from an exploded object. Curious
    example
    of this risk cropped up a while ago when bits from a Russian object caused people on the ISS to take shelter just in case some impacted.

    Jim

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  • From williamwright@21:1/5 to All on Wed Apr 20 17:45:04 2022
    On 20/04/2022 08:49, Brian Gaff (Sofa) wrote:
    The Iss and its controllers do have radar looking many miles ahead so they can make course changes to avoid this sort of thing, but its the bits
    smaller than you can see that are the danger.
    For a while old Long March rocket bodies had a tendency to explode several years after they had been used, and of course this spreads tiny bits through several orbits, however, at 22,400 miles out, its still relatively clear of this hazard. That is not to say of course that malicious intent might cause problems at that altitude if a weapon was sent there. It has been demonstrated that a relatively small laser weapon can disable a satellite at quite long ranges. They do not have to blow it up, just hit something important.
    As we know several nations have misguidedly used fragmentation techniques to destroy various in orbit objects and thus create hazards for many other spacecraft. There is active research going on on cost effective ways to
    clear such particles, but however you do it you are bound to miss some.
    I remember when I could still see a bit seeing pictures of areas of the outside of the ISS where there were dings and dents and scrapes where tiny objects had hit it. Thus far no serious damage has been done but some handrails have had to be changed due to sharp edges of dings damaging the silicon on astranaughts gloves.
    They are normally covered in RTV compound for better grip.
    I think the only incident that was down to impact damage was an ammonia leak in a radiator, which had to be replaced.

    Brian


    Interesting

    Bill

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  • From Jim Lesurf@21:1/5 to briang1@blueyonder.co.uk on Wed Apr 20 10:39:55 2022
    So does a certain Nation/Leader who recently disintegrated an object, with
    the fragment paths then risking a collision with the ISS. That the ISS
    would not have been able to 'dodge' the results by changing orbit
    sufficiently in time would also be known.

    Same Nation/Leader whose 'vistors' came to admire British Cathederals as
    while ago. And who more reently has sent troops to have a jolly time in Europe... erm, sorry, police action.

    Jim

    In article <t3odv4$1fo$1@dont-email.me>, Brian Gaff \(Sofa\) <briang1@blueyonder.co.uk> wrote:
    The Iss and its controllers do have radar looking many miles ahead so
    they can make course changes to avoid this sort of thing, but its the
    bits smaller than you can see that are the danger.

    --
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