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2
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10244249009
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-
M. J. S. Belton et al., ibid., p. 413; K. P. Klaasen et al., Opt. Eng. 23, no. 3, 334 (1984). The effective wavelengths of the SSI filters are dependent on the spectrum of the target. We name the filters according to their effective wavelength for integrated sunlight: Clear (628 nm); violet (414 nm); green (559 nm); red (664 nm); 731, 757, and 888 nm; and 1 μm (990 nm). Where the effective wavelengths differ appreciably for a given target we have noted the appropriate wavelength in the text.
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4
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10244250174
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note
-
The Galileo spacecraft achieved orbit on 7 December 1995. Although images of lo, Europa, and Jupiter were scheduled to be taken near this time, most of these were not recorded because of a tape recorder malfunction on 11 October 1995, just following the acquisition of the first Jupiter approach images. These Jupiter images remain on the tape but in a region that cannot be safely accessed. Galileo's central computer was reprogrammed partly to provide an essential capability to compress SSI images before their transmission to Earth on the spacecraft's law-gain antenna.
-
-
-
-
5
-
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10244263304
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-
note
-
According to the initial spacecraft operational flight rules, only one pass through the tape recorder was to be allowed following the Ganymede 1 encounter. This would have limited the number of returned images to about 117 and excluded most of the Europa coverage. However, because of technical problems with other experiments, four such passes were performed.
-
-
-
-
7
-
-
10244244787
-
-
note
-
The Galileo nominal mission, which ends on 31 December 1997, after 10 orbits, should return about 1500 images. However, the option exists with the current predictions for propellent usage and lifetime against failure due to radiation damage to extend the mission by 2 years. The SSI has examined a concept (the Galileo Europa Mission) that would return an additional 1500 images, mainly of Europa but also including very high resolution images (∼10 m per pixel) of lo not possible during the prime mission.
-
-
-
-
8
-
-
10244277846
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-
note
-
SSI was allotted 46 and 23% of the tape recorder space and downlink capability; of this, the Ganymede observations were allotted 47 and 51%, respectively.
-
-
-
-
9
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10744223899
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The initial Voyager imaging is reported in B. A. Smith et al., Science 204, 951 (1979), and B. A. Smith et al., ibid. 206, 927 (1979).
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The initial Voyager imaging is reported in B. A. Smith et al., Science 204, 951 (1979), and B. A. Smith et al., ibid. 206, 927 (1979).
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The new capabilities that were used in the sequence are (i) a modified 2 by 2 pixel summation mode that includes pre-exposure light flood (primarily used for Jupiter atmospheric images), (ii) a half-frame readout mode (used primarily for lo monitoring) and (iii) an Integer Cosine Transform (ICT) data compression routine. ICT was applied to all atmospheric images and most satellite images; for the highest resolution images, the SSI hardware compressor [BARC, or "Block Allocation Rate Controlled," R. F. Rice et al., Proc. National Telemetering Conference, Washington, DC, (1979)] was used in the rate-controlled mode.
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Proc. National Telemetering Conference
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Rice, R.F.1
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-
The exposure fault was discovered from the Europa mosaics, which were found to be underexposed by about a factor of 2 relative to predictions. This problem is understood and is being corrected. The BARC compressor problem, which is still not completely understood, was made evident by the large photometric contrast at high spatial frequencies seen in the Uruk Sulcus and Galileo Regio images of Ganymede. The compressor works by first truncating up to three least significant bits (LSBs) per pixel in an image line and then, if the compression achieved is not sufficient, truncating the last pixels' readout in a line. The photometric activity in these pictures was such that the compressor was pushed into truncating lines. Examination of the LSBs showed that the compressor did not consistently first truncate them to the three bit level. As a result, these images suffer from shortened lines, from the normal 800 samples per line to about 540.
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For studies of jovian cloud structure, see D. Banfield et al., Icarus, in press; F. M. Flasar et al., J. Geophys. Res. 86, 8759 (1981); R. A. West et al., Icarus 65, 161 (1990).
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note
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We thank the current project manager, W. J. O'Neil, and his predecessors J. R. Casani and R. J. Spehalski for their leadership; T. Brady and J. Marr for flight software development and its implementation; G. Levanas and his team for their diagnosis of the tape recorder problems and the creation of a safe way to operate this device; and W. Cunningham and his team who provided the new SSI camera flight software. T. Becker, E. Lee, R. Sucharski, and T. Rosanova provided the team with maps. Many associates of the team members contributed to the success of the SSI experiment; we thank N. Ausman, E.A. Alvarez del Castillo, K. Bender, H. Breneman, K. Buxbaum, T. Colvin, D. Deats, T. Denk, S. Fagents, A. Di Cicco, P. Helfenstein, S. Henderson, K. Homan, T. Jones, J.M. Kaufman, R. Krk, J. Klemaszewski, S. LaVoie, E. Lo, L, Lowes, K. Magee, W. Merline, R. Mitchell, H. Mortensen, B. Paczkowski, C. Phillips, K. Rages, A. Simon, D. Smonelli, J.N. Spitale, C. Stanley, E. Ustinov, D. Winther, D. Johnson, J. Van der Woude, J. Yatteau, A. Culver, D. Jensen, D. Alexander, and J. Yoshimizu. We acknowledge the contributions of absent colleagues H. Masursky, J. Pollack, C. Yeates and J. Dunne. A portion of this research was carried out by the Jet Propulsion Laboratory, California Institute of Technology, under contract with NASA. The National Optical Astronomy Observatories are operated by the Association of Universities for Research in Astronomy (AURA), under cooperative agreement with the National Science Foundation.
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