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Use of Thermal Reradiative Effects in Spacecraft Attitude ControlThermal reradiation effects on oscillation damping for spacecraft attitude control
Document ID
19660018458
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Peterson, C. A. (M.S. THESIS)
Date Acquired
August 3, 2013
Publication Date
May 1, 1966
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-CR-75450
CSR-T-66-3
Report Number: NASA-CR-75450
Report Number: CSR-T-66-3
Accession Number
66N27748
Funding Number(s)
CONTRACT_GRANT: NASR-249
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
VIBRATION DAMPING
OSCILLATION
SPACECRAFT CONTROL
ATTITUDE CONTROL
THERMAL RADIATION

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