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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.

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At least 307 records · Page 17

Galileo System Design for Orbital Operations

In April 1991, Galileo's X-band high gain antenna failed to deploy. An alternate approach which utilizes the spacecraft's S-band low gain antenna was conceived and is in development.

Galileo↗

Initial Galileo Propulsion System In-Flight Characterization

The Galileo RetroPropulsion Module (RPM) has performed excellently throughout the first three years of mission operations. The RPM is a state-of-the-art, pressure-fed, bipropellant propulsion system, provided to NASA by the Federal Republic of Germany.

Galileo↗

Automated Operations for Galileo Communications

After the Galileo High Gain Antenna (HGA) failed to deploy in 1991, the Jet Propulsion Laboratory(JPL) faced the challenge of implementing a science-rich mission with a Low-Gain Antenna (LGA), at data rates that were almost four orders of magnitude less than originally planned.

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Europa's Differentiated Internal Structure: Inferences from Two Galileo Encounters

Doppler data generated with the Galileo spacecraft's radio carrier wave during two Europa encounters on 19 December 1996 (E4) and 20 February 1997 (E6) were used to measure Euroapa's external gravitational field. The measurements indicate that Europa has a predominantly water ice-liquid outer shell about 100 to 200 klilometers thick and a deep interior with a density in excess of about 4000 kilograms per cubic meter.

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Galileo Europa Mission (GEM) Tour Design

The orbital tour trajectory that was selected for the Galileo mission includes ten close flybys of the Galilean satellites Europa, Ganymede, and Callisto, additional distant flybys of these satellites, lo torous observations, and many other events that provide broad opportunities for scientific observations.

Galileo↗

Galileo Telecom Link and its Application to Future Missions

On May 23, 1996, Galileo successfully switched to a new telecommunication mode with upgraded software on the spacecraft and comprehensively revised ground equipment. The new link offers multiple techniques (arraying, error-correcting coding, data compression, etc) to maximize the data return, while applying automation to minimize the complexity and cost of operations.

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Galileo's Telecom Using the Low-gain Spacecraft Antenna

Galileo's accomplishment of a science-rich mission through a low-gain antenna was made possible by a coordinated efforts of the Deep Space Network Support team, the spacecraft designers, and the science principal investigators.

on-board↗

Galileo Infrared Observations of Jupiter

Galileo infrared observaitons of Jupiter have been perfomed with two instruments, the Near Infrared Mapping Spectrometer (NIMS) and the Photo-Polarimeter Radiometer (PPR).

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Project Galileo Completing its Primary Mission

During this past year, the Galileo Orbiter has performed the large majority of its primary scientific mission in the Jupiter System-eigh of the eleven orbits and seven of the ten close satellite encounters and the deep penetration of the magnetotail.

Galileo↗

Galileo Orbiter Ultraviolet Observations of Jupiter Aurora

In 1996 during the first four orbits of the satellite tour the Galileo ultraviolet spectrometer (UVS) (1130-4320 A) and extreme ultraviolet spectrometer (EUVS)(540-1280 A) performed near-simultaneous observations of the Jupiter aurora in both the north and south polar regions.

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