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  • SPACE SCIENCES  (2)
  • SPACECRAFT DESIGN, TESTING AND PERFORMANCE  (2)
  • SPACECRAFT INSTRUMENTATION  (1)
  • 1
    Publication Date: 2011-08-19
    Description: The Galileo Mission and Spacecraft design impose tight requirements on the Attitude and Articulation Control System (AACS). These requirements, coupled with the flexible spacecraft, the need for autonomy, and a severe radiation environment, pose a great challenge for the AACS designer. The resulting design and implementation are described, along with the discovery and solution of the Single-Event Upset problem. The status of the testing of the AACS in the Integration and Test Laboratory as well as at the spacecraft level is summarized.
    Keywords: SPACECRAFT DESIGN, TESTING AND PERFORMANCE
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  • 2
    Publication Date: 2011-08-19
    Description: The Galileo mission and spacecraft, consisting of a Jupiter-orbiter and an atmospheric entry probe, are discussed. Components will include: magnetometers and plasma-wave antennas on a boom, high-gain antenna, probe vehicle, two different bus electronics packages, and a radioisotope thermoelectric generator. Instruments, investigators and objectives are tabulated for both probe science and orbiter science investigations. Requirements in the design of the attitude and articulation control system are very stringent because of the complex dynamics, flexible body effects, the need for autonomy, and the severe radiation environment in the Jupiter nighborhood. Galileo was intended to be ready for launch via Space Shuttle in May of 1986.
    Keywords: SPACECRAFT DESIGN, TESTING AND PERFORMANCE
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  • 3
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    In:  Other Sources
    Publication Date: 2019-07-13
    Description: Research concerning flight computers for use on interplanetary probes is reviewed. The history of these computers from the Viking mission to the present is outlined. The differences between ground commercial computers and computers for planetary exploration are listed. The development of a computer for the Mariner Mark II comet rendezvous asteroid flyby mission is described. Various aspects of recently developed computer systems are examined, including the Max real time, embedded computer, a hypercube distributed supercomputer, a SAR data processor, a processor for the High Resolution IR Imaging Spectrometer, and a robotic vision multiresolution pyramid machine for processsing images obtained by a Mars Rover.
    Keywords: SPACECRAFT INSTRUMENTATION
    Type: International Symposium on Space Technology and Science; May 22, 1988 - May 27, 1988; Sapporo; Japan
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  • 4
    Publication Date: 2019-07-13
    Description: System analysis to determine orbital parameters influence on mission scientific objectives under engineering constraints, using value function
    Keywords: SPACE SCIENCES
    Type: AIAA PAPER 68-1052 , AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, ANNUAL MEETING AND TECHNICAL DISPLAY, 5TH; Oct 21, 1968 - Oct 24, 1968; PHILADELPHIA, PA|; STITUTION OF ENGINEE
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  • 5
    Publication Date: 2019-07-13
    Description: System analysis to determine orbital parameters influence on mission scientific objectives under engineering constraints, using value function
    Keywords: SPACE SCIENCES
    Type: AIAA PAPER 68-1052 , ANNUAL MEETING AND TECHNICAL DISPLAY; Oct 21, 1968 - Oct 24, 1968; PHILADELPHIA, PA
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