Galileo Plans for Shoemaker-Levy 9 Observations
The Galileo spacecraft will have the best direct view of the predicted S-L 9 impact sites of any observing platform.
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The Galileo spacecraft will have the best direct view of the predicted S-L 9 impact sites of any observing platform.
Due to a malfunctioning high-gain antenna, the Galileo spacecraft is transmitting all its data through a low-gain antenna, and the data rate will seldom exceed 100 bits per second during its two-year tour of Jupiter's satellites.
During the August 28, 1993 Galileo flyby of 243 Ida, the Near Infrared Mapping Spectrometer experiment obtained spectral images in the wavelength range 0.7 - 5.2 um.
In this paper we describe the advanced source and channel coding schemes that we plan to use to enhance the data return from the crippled Galileo spacecraft.
The Galileo spacecraft is currently on its way to Jupiter and its moons. In April 1991, the high gain antenna (HGA) failed to deploy as commanded.
Radiometric tracking Doppler measurements of the signal transmitted by the Galileo spacecraft using an Ultra-Stable Oscillator (USO) as a frequency reference have been acquired by antennas of the NSA Deep Space Network between Dec. 1998 and No. 1991.
This paper describes the performance of Full-Spectrum Combining (FSC), an arraying technique being considered for the Galileo S-Band Mission.
...This paper presents results from a demonstration of a new sequential filter model and data reduction technique, dubbed the enhanced filter, performed with radio tracking data obtained from the Galileo spacecraft.
During September and October 1991, pictures of the Gaspra asteroid and neighboring stars were taken by the Galileo Optical Navigation (OPNAV) Team for the purpose of navigation the spacecraft for a successful Gaspra encounter. The star tracks in these pictures showed that the scan platform celestial pointing cone controller performed poorly in compensating for wobble-induced cone offsets.
A recent failure of Galileo's magnetic recorder was identified as LED degradation. Annealing the culprit OP133s proved successful and the irreplaceable data was recovered. Test data and modeling results calibrate an understanding of this incident.
Measurements of the high energy, omni-directional electron environment by the Galileo spacecraft Energetic Particle Detector (EDP) were used to develop a new model of Jupiter's trapped electron radiation in the jovian equatorial plane for the range 8 to 16 Jupiter radii.
The Galileo spacecraft's navigation results for the first eleve Jupiter satellite encounters are described.
This document establishes the functional requirements of the Galileo Orbitor plasma wave subsystem (PWS) which is used to investigate electric and magnetic waves in space plasmas.
Radio metric data from the Pioneer 10/11, Galileo, and Ulysses Spacecraft indicate an apparent anomalous, constant, acceleration acting on the spacecraft with a magnitude ~8.5 x 10(sup -8) cm/s(sup 2), directed towards the Sun.
The radio signal from the Galileo prove to the orbiter experienced attenuation due to ammonia in Jupiter's atmosphere during the probe descent.
At this very moment, spacecraft Galileo is orbiting the planet Jupiter. We invite you to join us for an exciting 2-year mission, the first extensive visit to an outer planet and its satellites.
The Galileo spacecraft will use a Near Infrared Mapping Spectrometer (NIMS) to study Jupiter s moon, Ganymede. Although the main goal is to study the chemical components in the various surface compositional units, terrain types, craters, polar effects, hemisphere differences, and the atmosphere also will be examined.
A primary objective of the Galileo mission is to investigate Io s vulcanism. The NIMS combines imaging and spectral capabilities to map Io s surface and plumes.