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The most famous sustained arc event of all led to the breakage of the TSS-1R electrodynamic tether, and the loss of the attached satellite. Figure 8 shows the burned, frayed and broken tether end still attached to the Shuttle after the break. Incidentally, the tether continued arcing long after it and its satellite were drifting free, until finally it went into night conditions where the electron density was insufficient to sustain the arc
Originally posted by WitnessFromAfar
Zorgon is this what you meant to post earlier? The nasas-unknowns.com link is a dead one for me... Thank you for posting the content though, from where-ever it was you were trying to link!
Originally posted by WitnessFromAfar
Try 'save target as' to get the .pdfs for the other two!
You are denying the simple explanation, trying to obfuscate the issue. There is nothing mysterious about the "glow" and floaters. How many people have posted videos and images of disks, even with notches, made filming small out of focus lights at night?
Any examples, supporting evidence? I would like to grasp your concepts of false parallax, glowing polarized static charges, and your theory about water and ice not being able of hold a static charge. Do you deny that static charges are involved in lightning? Are clouds not water and ice?
I can not prove this, it is only one of my theories.
I don't understand why the static charges, polarized or not would be visible. If you think some sort of plasma surrounds objects in space, you have a lot more explaining to do.
A question: do you have an alternate theory about everything? Is there anything about mainstream physics that you agree on? I mean, if we have no common ground, there is no point discussing anything.
Thank you for your patience, and don't take me wrong, You, Armap and Balez (and other posters) have all my respect for your research on the subject.
Originally posted by Balez
1.....2.....3 seconds the shuttle has travelled 14,166 miles since ejection.
Why is the tether visible as it is?
Same here, whatever it is we are discussing, we are trying to find a solution to a problem, we wont do that if we become unfriendly to each other.
Don't take me wrong, i love to discuss, there really is not much else in life that you gain so much from as discussing things, sometimes i can discuss just because of the discussion, not because i have something to prove, but to learn.
Jettisoned debris would travel the same amount, more or less, unless they somehow instantly stop as soon as they are ejected. Why would they stop or even quickly decelerate?
You must be right about the tether. The ionosphere is a plasma, basically, but it should only glow when there's an electrical discharge AFAIK. My (very limited) understanding is: there's a difference of potential between the ionosphere at the two extremities, assuming the tether is still vertical. Shouldn't the extremities of the tether glow, then, as in the well known corona discharge phenomenon? I admit I don't understand.
Please accept my apology for my bad manners. It was not my intention, really. Hey, even my horoscope says everyone I meet today will suffer for my temper.
Originally posted by Balez
Yes if they are in a constant (the shuttle) that is true, but when they get jettisoned, or ejected, their momentum change, now they are no longer at a constant with the shuttle.
When this happens they also get a different trajectory than the shuttle.
There are more than 50 sources of ice on the shuttle, plus a steady source of debris such as insulation flakes from inside the payload bay. This includes 38 primary RCS jets and 6 vernier jets (which burn the hypergolic [self-igniting] propellants of nitrogen tetroxide and hydrazine), an air dump line, a waste water dump line, a supply water dump line, two fuel cell purge lines (the hydrogen one is always leaking water), two flash evaporators, a water spray boiler, and so forth. No surprise, then, that floating debris near the shuttle is a common sight. The particles usually (not always) spin, and depending on the axis of spin they may or may not flash, and depending on the speed of spin their flicker may or may not be picked up by the camera CCD scanner.
Originally posted by nablator
Originally posted by Balez
Yes if they are in a constant (the shuttle) that is true, but when they get jettisoned, or ejected, their momentum change, now they are no longer at a constant with the shuttle.
When this happens they also get a different trajectory than the shuttle.
Thanks for explaining. So you assume the debris are always thrown out into space with significant speed relative to the shuttle. That would be the case with RCS thrusters, but not with other sources of debris: leaks, dumps, etc.
Quoted from a STS-48 UFO video debunking article:
There are more than 50 sources of ice on the shuttle, plus a steady source of debris such as insulation flakes from inside the payload bay. This includes 38 primary RCS jets and 6 vernier jets (which burn the hypergolic [self-igniting] propellants of nitrogen tetroxide and hydrazine), an air dump line, a waste water dump line, a supply water dump line, two fuel cell purge lines (the hydrogen one is always leaking water), two flash evaporators, a water spray boiler, and so forth. No surprise, then, that floating debris near the shuttle is a common sight. The particles usually (not always) spin, and depending on the axis of spin they may or may not flash, and depending on the speed of spin their flicker may or may not be picked up by the camera CCD scanner.
This is about STS-48, but why would STS-75 be different?
[edit on 2008-3-31 by nablator]
Thanks for explaining. So you assume the debris are always thrown out into space with significant speed relative to the shuttle. That would be the case with RCS thrusters, but not with other sources of debris: leaks, dumps, etc.
two flash evaporators, a water spray boiler, and so forth. No surprise, then, that floating debris near the shuttle is a common sight.
Originally posted by cams
NASA: "Franklin, We see a long line, couple star like things and alot of things swimming in the foreground, can you describe what you are seeing?"
Astronaut: "Well the long line is the tether um and there is a little bit of debris that ah kind of flies with us - and it's illuminated by the sun...."
Originally posted by zorgon
As to that other non working link... yeah its no longer available... (that happens a LOT lately when seeking answers... vanishing pages)
HOWEVER, Google cache sometimes yields gems
None of them change directions. When the shuttle fires its thrusters every one of them moves, or when the camera zooms in they "move".
This is very simple. And yes, they will "fly" with the shuttle untill the shuttle accelerates away. This is space remember. There are no anomalies, that is what dust in space looks like.
An electrodynamic tether is essentially a long conducting wire extended from a spacecraft. The gravity gradient field (also known as the "tidal force") will tend to orient the tether in a vertical position. If the tether is orbiting around the Earth, it will be crossing the Earth's magnetic field lines at orbital velocity (7-8 km/s!). The motion of the conductor across the magnetic field induces a voltage along the length of the tether. This voltage can be up to several hundred volts per kilometer.
In an "electrodynamic tether drag" system, such as the Terminator Tether, the tether can be used to reduce the orbit of the spacecraft to which it is attached. If the system has a means for collecting electrons from the ionospheric plasma at one end of the tether and expelling them back into the plasma at the other end of the tether, the voltage can drive a current along the tether. This current will, in turn, interact with the Earth's magnetic field to cause a Lorentz JXB force which will oppose the motion of the tether and whatever it is attached to. This "electrodynamic drag force" will decrease the orbit of the tether and its host spacecraft. Essentially, the tether converts the orbital energy of the host spacecraft into electrical power, which is dissipated as ohmic heating in the tether.
In a "electrodynamic propulsion" system, the tether can be used to boost the orbit of the spacecraft. If a power supply is added to the tether system and used to drive current in the direction opposite to that which it normally wants to flow, the tether can "push" against the Earth's magnetic field to raise the spacecraft's orbit. The major advantage of this technique compared to other space propulsion systems is that it doesn't require any propellant. It uses the Earth's magnetic field as its "reaction mass." By eliminating the need to launch large amounts of propellant into orbit, electrodynamic tethers can greatly reduce the cost of in space propulsion.
An electrodynamic tether is a long wire orbiting in the Earths magnetic field that uses the electric field generated by its motion, the so-called lvrrr•×B theof field (where tetherlength theis l and field, magnetic theis velocity, theis vrrrBor structure), to produce power or propulsion. This concept was proved on orbit by the PMG experiment, where both modes of operation were produced by emitting electrons (by means of plasma contactors) either at the top or bottom of a 500-meter tether to produce power (electron emission at the bottom) or propulsion (electron emission at the top). The maximum Brr×v on a structure in LEO is about 1/3 volt per meter.
EARLY FINDINGS FROM TETHERED SATELLITE MISSION
POINT TO REVAMPING OF SPACE PHYSICS THEORIES
RELEASE: 96-43
Numerous space physics and plasma theories are being revised or overturned by data gathered during the Tethered Satellite System Reflight (TSS-1R) experiments on Space Shuttle Columbia’s STS-75 mission last March.
Models, accepted by scientists for more than 30 years, are incorrect and must be rewritten. This assessment follows analysis by a joint U.S.-Italian Tethered Satellite investigating team of the information gathered during the mission.
TETHERED SATELLITE INVESTIGATION REPORT IS RELEASED
Italian Space Agency (ASI)
Excerpt
NASA and the Italian Space Agency today released the report of the investigative board appointed to determine factors which resulted in the Feb. 25 tether break and loss of the Tethered Satellite during the STS-75 Space Shuttle mission.
Findings of the board, included in a 358-page document, identified primary causes which accounted for the tether break during deployment of the Tethered Satellite.
The tether failed as a result of arcing and burning of the tether, leading to a tensile failure after a significant portion of the tether had burned away," the report concludes. The arcing occurred because either external foreign object penetration (but not orbital debris or micrometeoroids) or a defect in the tether caused a breach in the layer of insulation surrounding the tether conductor. The insulation breach provided a path for the current to jump, or arc, from the copper wire in the tether to a nearby electrical ground...
Excerpt
The tether was designed to carry up to 15,000 volts DC and handle tensile forces of up to 400 pounds (1780 newtons). It used super-strong strands of Kevlar as a strength-providing member, wound around the copper and insulation. However, postflight inspection of the tether end which remained aboard Columbia showed it to be charred. The board concluded that after arcing had burned through most of the Kevlar, the few remaining strands were not enough to withstand forces being exerted by satellite deployment...