Design of the Galileo Satellite Tour
Concepts, strategies, and techniques developed in the 1970s and 1980s, which were used in designing the satellite tour for the 1986 launch opportunity were employed and extended for this effort.
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Concepts, strategies, and techniques developed in the 1970s and 1980s, which were used in designing the satellite tour for the 1986 launch opportunity were employed and extended for this effort.
The Sun-Jupiter Trojan asteroids are celestial bodies of great scientific interest as well as potential resources offering water and other mineral resources for longterm human exploration of the solar system. Previous investigations under this project have addressed the automated design of tours within the asteroid swarm. This investigation expands the current automation scheme by incorporating options for a complete trajectory design approach to the Trojan asteroids. Computational aspects of the design procedure are automated such that end-to-end trajectories are generated with a minimum of human interaction after key elements and constraints associated with a proposed mission concept are specified.
In this paper we investigate tours involving the Jovian satellites Europa, Ganymede, and Callisto for the Europa Orbiter mission.
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.
This slide is intended to serve as an informational display located on the machine high bay for visitors on Z tours. This display reflects some of our updated research capabilities that Z performs to support our nuclear deterrence mission.
Trajectory analysis of multiplanet Grand Tour mission to four large outer planets on single flight, discussing mission planning
Trajectory analysis of multiplanet Grand Tour mission to four large outer planets on single flight, discussing mission planning
Trajectories for 1976 to 1980 Grand Tours
Optimized solar electric low thrust propulsion and intermediate planetary swingby technique for grand tour missions to outer planets
Galilean satellites touring by Jupiter spacecraft, discussing orbit calculation and encounter geometry
Grand tours navigation system consisting of deep space network radio and onboard TV for future TOPS /Thermoelectric Outer Planet Spacecraft/ applications
Grand Tour mission design, discussing navigation, trajectory parameters, launch vehicles and satellite flybys
PCM TV photographic data communication for grand tour of outer planets, emphasizing adaptive information-preserving data compression system for optimal performance
Spacecraft computer centered data systems with standby redundancy, automated flexibility and LSI devices for grand tour mission
High energy fast Grand Tour multiplanet flyby missions to outer planets omitting Jupiter, noting identical arrival date at Neptune
IR experiments planning for Outer Planets Grand Tour including investigations of planetary radiation balance and atmospheric composition and satellites composition and physical properties
Multiplanet gravity assist grand tours in outer solar system, discussing launch opportunities and mission effects on spacecraft design
Grand Tour missions centralized data handling, describing computer aided telemetry system and self testing and repairing control computer