Spacecraft development

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Launch CampaignKourou, French GuyanaBaikonur, KazakhstanDeparture to launch siteThe S/C shall fit in its container thatshall fit within Antonov airplane
Final preparationPropellant fueling
Page 2 and 3: Gaia programme overview1995 - 2004:
Page 5 and 6: The specification treePArequirement
Page 7 and 8: Mechanical and electrical integrati
Page 9 and 10: Physical measurementsGaia on its ho
Page 11 and 12: Spacecraft design approach Although
Page 13 and 14: Gaia mechanical architecture Decoup
Page 15 and 16: Gaia thermal architectureDSA stowed
Page 17 and 18: Gaia AOCSGaia AOCSAstroStar tracker
Page 19 and 20: CCSVM MIL-STD-1553B Bus NGaia Commu
Page 21: Specific on Gaia: Timing architectu
Page 25 and 26: LaunchAnd spacecraft operations are
Page 27 and 28: General ApproachRequired performanc
Page 29 and 30: Major features of the study design
Page 31 and 32: Astro Beam (2/4)Astro Beam (3/4)
Page 33 and 34: APT Beam (1/4)APT Beam (2/4)
Page 35 and 36: Payload accommodationDimensions com
Page 37 and 38: GAIA mechanical modelGAIA mechanica
Page 39 and 40: Gaia configuration : 2002PLMSVMSuns
Page 41 and 42: 2002 Astrometric Instrument Configu
Page 43 and 44: 2002 FEM results: PLM eigenfrequenc
Page 45 and 46: Modal analysis resultsLateral mode
Page 47 and 48: Gaia configuration: 2005Satellite d
Page 49 and 50: Focal Plane Assembly A cold part at
Page 51 and 52: The mechanical SVM The thermal tent
Page 53 and 54: Torus designFPA design

Spacecraft development

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