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Understanding the Kepler Reaction Wheels & SatelliteFollowing the loss of two reaction wheels four years into its mission, the Kepler team was faced with reinventing an operational approach to continue to deliver compelling science using an unanticipated suite of actuators. Spacecraft thrusters were not designed for accurate pointing control, yet with only two reaction wheels, only two axes could be actively controlled. With solar pressure as the only disturbing force, and recognizing the innate symmetry of the spacecraft, the K2 mission points the spacecraft in the orbital plane for three months at a time, placing the antennas 90° from the earth. Mapping the solar balance ridge 70 M km from Earth, with limited communications and a reduced staff presented a significant operational challenge.
Document ID
20180007379
Acquisition Source
Ames Research Center
Document Type
Abstract
Authors
Sobeck, Charles K.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
November 1, 2018
Publication Date
May 28, 2018
Subject Category
Lunar And Planetary Science And Exploration
Report/Patent Number
ARC-E-DAA-TN55091
Meeting Information
Meeting: International Conference on Space Operations (Space Ops 2018)
Location: Marseille
Country: France
Start Date: May 28, 2018
End Date: June 1, 2018
Sponsors: Centre National d'Etudes Spatiales (CNES), American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 354171
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Engineering
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