The Galileo spacecraft system designThe Galileo Orbiter differs markedly from its Mariner, Viking and Voyager predecessors in many aspects of its design, as dictated by its unique mission characteristics. Novel design features include a dual spin configuration, long life bipropellant propulsion, radioisotope thermoelectric generators, and a star scanner. Other major changes are related to Space Shuttle Orbiter compatibility. The selection of a distributed data system employing a high speed data bus represents a major advance over Voyager systems. The command, control and data handling functions for the Orbiter are merged into a single software-controlled subsystem. The paramount importance of software development in the design of Galileo subsystems is noted, in view of the requirement for total engineering and science data acquisition process reprogrammability.
Document ID
19830036689
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Jones, C. P. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Landano, M. R. (California Institute of Technology, Jet Propulsion Laboratory, Spacecraft Systems Engineering Section, Pasadena CA, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1983
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 83-0097Report Number: AIAA PAPER 83-0097
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Aerospace Sciences Meeting