1984
DOI: 10.1117/12.7973290
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Charge-Coupled Device Television Camera For Nasa's Galileo Mission To Jupiter

Abstract: The slow -scan television camera being built for NASA's Galileo Jupiter Orbiter spacecraft consists of a 1500 mm focal -length telescope coupled to a camera head housing a newly developed 800 x 800 element charge -coupled device (CCD) detector based on "virtual-phase" charge transfer technology. This detector results in a broadband sensitivity over 100 times that of a comparable vidicon -tube camera while also yielding improved resolution, linearity, geometric fidelity, and spectral range. In the near -Jovian … Show more

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Cited by 31 publications
(17 citation statements)
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“…Results of these measurements are presented in Table II. Zharkov et al (1985) give an expression for the Love The C 22 Gravitational Coefficients of the Satellites number k 2 of a satellite as h 2 are given in Table II. Thus, it is possible to make more accurate and repeatable the Galileo Europa mission will more accurately define both their gravitational fields and shapes.…”
Section: Triaxial Equilibrium Ellipsoidsmentioning
confidence: 99%
See 1 more Smart Citation
“…Results of these measurements are presented in Table II. Zharkov et al (1985) give an expression for the Love The C 22 Gravitational Coefficients of the Satellites number k 2 of a satellite as h 2 are given in Table II. Thus, it is possible to make more accurate and repeatable the Galileo Europa mission will more accurately define both their gravitational fields and shapes.…”
Section: Triaxial Equilibrium Ellipsoidsmentioning
confidence: 99%
“…The pixel size is about 15 Ȑm for the Voyager of the coordinates, while the errors in z were generally smaller. The overdetermination was 2.2. cameras and 15.24 Ȑm for the Galileo camera (Davies et al 1979, Klaasen et al 1984.…”
Section: The Satellite Coordinate Systemsmentioning
confidence: 99%
“…Details of the solid-state imaging (SSI) experiment have been previously published by Klaasen et al [1984Klaasen et al [ , 1997 and Belton et al [1992]. As its name suggests, the SSI utilizes a solid-state charge-coupled device (CCD) detector attached to a telescope with a focal length of 1.5 m. The instantaneous field of view (IFOV) is 10 mrad, yielding a spatial resolution -50 times higher than NIMS.…”
Section: Galileo Nims and Ssi Observations Of Iomentioning
confidence: 99%
“…1 Originally J was set to 34. Based on the data from the first two orbits, our original model for the radiation noise rate was increased by a factor of 1.6 at 9.4R J and below transitioning to a factor of 1.4 at 15R J and above by changing the value of J to 54 below 9.4R J transitioning to 46 above 15R J .…”
Section: Jϭn/sqrt͑s ͒mentioning
confidence: 99%
“…1,2 A previous publication documented the SSI inflight calibration and performance characteristics and how they have evolved during the 6-yr cruise to Jupiter. 3 In this paper, we describe the performance of the SSI during Jupiter orbital operations.…”
Section: Introductionmentioning
confidence: 99%