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Altimeter and radiometer for a Venus orbiter missionThe concept, constraints, and capabilities of a radar altimeter type contour mapper for a Venus orbiter mission are presented. The system was developed for the proposed planetary explorer universal bus concept. A system with a height precision of 30meters over a surface area of 7200 square kilometers is achieved. Using this system and the orbit proposed in the orbiting bus concept, the northern hemisphere of Venus is mapped in one Venus day. The radar receiver system, is used in a radiometer mode to obtain a map of the diurnal and logitudinal variations of the Venus surface temperature with a resolution of 3.0 degrees Kelvin.
Document ID
19720007785
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Bryan, J. W.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Richter, K. R.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 2, 2013
Publication Date
December 1, 1971
Subject Category
Instrumentation And Photography
Report/Patent Number
NASA-TM-X-65795
X-551-71-494
Report Number: NASA-TM-X-65795
Report Number: X-551-71-494
Accession Number
72N15435
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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