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Radar imaging from a spinning spacecraftThe feasibility of imaging the surface of Venus using a synthetic aperture radar in a spin stabilized Pioneer class spacecraft operating in an eccentric orbit is studied. Imaging radar fundamentals, constraints, power requirements and data processing considerations are reviewed. Additional effects due to operation from an elliptical orbit with a spinning spacecraft are covered. Recommended spin parameters are determined by simulations. Extensions to include noncoherent integration and stereo coverage are briefly reviewed. The results indicate that resolution on the order of 100 meters can be obtained from a 0.2 eccentricity orbit using a 2 meter antenna and reasonable transmitter power levels.
Document ID
19760021364
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bayma, R. W.
(Environmental Research Inst. of Michigan Ann Arbor, MI, United States)
Hidayet, M. A.
(Environmental Research Inst. of Michigan Ann Arbor, MI, United States)
Date Acquired
September 3, 2013
Publication Date
March 1, 1976
Subject Category
Communications And Radar
Report/Patent Number
ERIM-115200-2-F
NASA-CR-137829
Report Number: ERIM-115200-2-F
Report Number: NASA-CR-137829
Accession Number
76N28452
Funding Number(s)
CONTRACT_GRANT: NAS2-8860
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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