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Venus wind-altitude radar studyA study was made of a wind/altitude radar for a Venus probe. The baseline configuration was taken to be the SKD-2100 Doppler radar modified to accommodate the altimeter portion of the APN-187 and a single beam antenna. Using current models of the Venus environment, engineering studies were made to define design requirements and to estimate the operational and physical characteristics of the conceptual design. The results of the study are that: (1) the radar instrument should have an altitude limit of at least 34 km for velocity and at least 17.5 km for altitude measurement, (2) vertical accuracy should be better than + or - 0.9 percent and horizontal velocity accuracy should be better than + or - 3 percent over the operating altitude range, and (3) altimeter accuracy should be within + or - 3 percent up to about 2.5 km and should improve over the remainder of the altimeter operating range. The radar is expected to require between 48.5 and 69.3 watts of power and to weigh between 3.86 and 5.21 kg (8.5 and 11.5 lb). In each case, if power could be supplied directly from the probe batteries the lower figures would apply; the upper figures would apply if a power conditioner must be used.
Document ID
19730017144
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Goldfischer, L. I.
(Singer-Kearfott Pleasantville, NY, United States)
Date Acquired
August 7, 2013
Publication Date
January 1, 1973
Subject Category
Space Sciences
Report/Patent Number
Y256E012
NASA-CR-114556
Report Number: Y256E012
Report Number: NASA-CR-114556
Accession Number
73N25871
Funding Number(s)
CONTRACT_GRANT: NAS2-7255
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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