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TSS-1R mission responsibilities are shared between the Marshall and Johnson Centers, with ASI support at each location. Marshall provides project management, as well as system development, testing and integration. Science teams work under Marshall direction. Marshall will furnish real-time engineering support for the TSS-1R system components and tether dynamics. All remote commanding of science instruments aboard the satellite deployer and the Tethered Satellite will be executed by the Marshall Payload Operations Control team. Because of the unique interaction between the payload and the Shuttle, Mission Control in Houston is responsible for the crew's deployment and retrieval of the satellite. Mission Control also will manage the satellite in orbit and monitor the state of the instrument pallet, the deployer and the satellite. ASI will provide equipment engineering support during the mission.
TSS-1R is directed by Program Manager Tom Stuart, Office of Space Flight, and Science Payload Program Manager Mike Calabrese, Office of Space Science, NASA Headquarters, Washington, DC. Responsible for project management at Marshall are Mission Manager Robert McBrayer and Mission Scientist Dr. Nobie Stone, who also serves as project scientist and co-chairman of the Investigator Working Group. The chief engineer is Tony Lavoie. At the Italian Space Agency, Rome, Italy's TSS-1R contribution is directed by ASI Program Manager Dr. Carlo Bonifazi, also the ASI Science Program Manager. Responsible for the Project Management of the satellite and the Core Equipment are, respectively, Raffaele Battaglia and Francesco Svelto. Dr. Marino Dobrowolny is ASI Mission Scientist, with his assistant Dr. Jean Sabbagh.
Originally posted by mcrom901
Originally posted by JimOberg
Just got the response from NASA PAO with the Execute Package for the day of the tether video.
where is the more relevant msg no# 101 - fd08 tss science update
The tether broke near full deployment (19 km) on 26 Feb at 01:30 UT. The initial orbit for the satellite was 316 x 413 km; meanwhile the shuttle was at 291 x 299 km. The break was due to an electrical shortcut inside the cable.
Loss of NASA/ASI tethered satellite cause by debris.(Italian Space Agency)
Defense Daily | June 6, 1996| Ahles, Andrea
U.S. and Italian space agency officials have concluded that debris caused the loss of the joint NASA and Italian Space Agency (ASI) Tethered Satellite in February.
After a four-month investigation, space officials found that debris sliced through the insulation of the tether--that connected the satellite to the Space Shuttle orbiter--and caused a short that burned through the pencil-thin cable.
The anomalies located with radiography were flagged for removal from the tether and analysis. The anomaly shown in Figure 1 was found to consist of several contaminants that may have been introduced during production or handling of the tether.
Figure 1 - Radiographic image of tether showing anomalous material suspended in Kevlar braid. The dimensions of the inclusion are approximately 1.5 x 1.0 mm (0.06 x 0.04in.). This radiograph was produced using the lower energy technique, which did not penetrate the copper strands.
A radiograph of the failed end is shown in Figure 2. Evidence of melting in the copper strand and the surrounding FEP insulation was evident from radiographs of the failed end. This corroborated other visible evidence that the tether failure resulted from excess arcing between the tether and the ambient environment.
Figure 2 - Radiograph of the failed end of the TSS-1R tether. The broken and melted ends of several copper strands and melted FEP insulation are visible.
Beyond the initial 27 m (89 ft) segment, approximately 1,800 m (5,900 ft) of tether remained on the payload bay reel after separation. The remaining tether was also brought to MSFC for analysis. Thirty random locations along the longer segment were selected for radiographic analysis, as well as three anomalies that were noted during visual inspection. The analysis of the 1,800 m (5,900 ft) segment showed that it contained far less particulate contamination than the failed end, which would be consistent with the conclusion that arcing had occurred at the location of the separation.
Originally posted by mcrom901
[atsimg]http://files.abovetopsecret.com/images/member/953377b2ec24.jpg[/atsimg]
recoiling after breaking free.....
i.e. the observed diameter not being henceforth the 'virgin' 2.54 mm....
Originally posted by JimOberg
Originally posted by mcrom901
Originally posted by JimOberg
It also fails because the tether was visually observed, both by the crew and by ground observers, to be long, thin, and straight, except a few days later the bottom few miles slightly curved (due to air drag). There was no corkscrew-curlicuing seen, and the human eye is a much more precise angular and detail resolution instrument.
your comments make no sense..... what do you mean by 'thin'.... how thin?
'Thin' meant no observed thickness at all -- a linear equivalent of a point source. It had been debated how visible the line, with the thickness of a telephone cord, would be from a range of several hundred miles. Because of the maximum contrast -- bright white against black background -- there were sufficient photons from the thin line to register unambiguously both on eyeballs and optics.
I have been an astronomer for 40 years and a satellite observer for 36. I really got into satellite observing while under the wing of fellow San Antonio resident, Paul Maley, while we were both still in high school here in Texas in 1961. In all the years since, I have not seen a satellite pass to compare with this morning's TSS pass over San Antonio, Texas. It was stunning! I am still amazed after thinking about it for four hours.
TSS popped out of the shadow at 5:53 AM, local time and lit up like a neon sign. It was fully three degrees long with the TSS itself easily visible as a 3 to 3.5 mag point of light at the upper end of the bluish-gray tether. The tether was angled at a position angle (to local vertical) of about 220 degrees and at the lower (snapped-off) end was a noticable condensation of light. It was obviously coiled slightly at the free end.
I am assuming that for the tether to be so visible, it must be coiled like a telephone cord and have more "width" than just the 2.5 mm thickness of the cord.
Originally posted by mcrom901
furthermore.... observation of orbs near other satellites...... 03.96....
Cosmos 1933 + other obs
Here are a few recent observations.
[]
www.satobs.org...
Originally posted by depthoffield
If this light is captured with a lens/mirros, and make images on a senzor (CDD or whatever), (which senzor in this case is a special CCD with a coating to increase efficency), then making the image with light follow the same rule of optics...including focusing.
By using the TOP images to make measurements of the visible light radiated by the plasma, this process, and how it affects the spacecraft, can be better understood.
Originally posted by mcrom901
irrespective of the cameras capabilities in regards to the visible spectrum (or near).... the main point of focus here is the source of light.....
Originally posted by mcrom901
check these...
I have been an astronomer for 40 years and a satellite observer for 36.
[]
TSS popped out of the shadow at 5:53 AM, local time and lit up like a neon sign. It was fully three degrees long with the TSS itself easily visible as a 3 to 3.5 mag point of light at the upper end of the bluish-gray tether. The tether was angled at a position angle (to local vertical) of about 220 degrees and at the lower (snapped-off) end was a noticable condensation of light. It was obviously coiled slightly at the free end.
The source of light is the tether illuminated by the sunlight. Direct witnesses said that.
Jim Oberg is one, but it seems from some speakers here, he must lie because worked for NASA.
Originally posted by depthoffield
The source of light is the tether illuminated by the sunlight. Direct witnesses said that.
Jim Oberg is one, but it seems from some speakers here, he must lie because worked for NASA.
Originally posted by depthoffield
NASA camera C, a low light camera, saw the sunlit tether, not a plasma ultraviolet thing. While TOP camera was special designed in this mission to be used on the tether experiments, this 1 march 1996 encounter with the tether (and the "UFO's here) was filmed by NASA camera C, not by the TOP camera. Why you continue to speak about TOP camera, since not the TOP camera filmed this UFO's, but a visible spectrum camera ?
Originally posted by Phage
reply to post by mcrom901
Many people observed the tether.
www.satobs.org...
that Oberg was lying.
Originally posted by easynow
The source of light is the tether illuminated by the sunlight. Direct witnesses said that.
you do not know if there are other reasons the tether was "illuminated"
Originally posted by easynow
also anyone that does not agree that we need to see NASA's copy of the STS75 video is straight up dis info.