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Space Shuttle Proximity Operation Sensor StudyThe performance of the Kuband radar was analyzed in detail, and the performance was updated and summarized. In so doing, two different radar design philosophies were described, and the corresponding differences in losses were enumerated. The resulting design margins were determined for both design philosophies and for both the designated and nondesignated range modes of operation. In some cases, the design margin was about zero, and in other cases it was significantly less than zero. With the point of view described above, the recommended solution is to allow more scan time but at the present scan rate. With no other changes in the present configuration, the radar met design detection specifications for all design philosophies at a range of 11.3 nautical miles.
Document ID
19780010175
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Weber, C. L.
(Axiomatix Los Angeles, CA, United States)
Alem, W. K.
(Axiomatix Los Angeles, CA, United States)
Date Acquired
September 3, 2013
Publication Date
February 15, 1978
Subject Category
Spacecraft Instrumentation
Report/Patent Number
NASA-CR-151634
AXIOMATIX-R7802-2
Report Number: NASA-CR-151634
Report Number: AXIOMATIX-R7802-2
Accession Number
78N18118
Funding Number(s)
CONTRACT_GRANT: NAS9-15502
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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