NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Windshear radar calibration: Transmitter power and receiver gain stabilityAn experimental windshear Doppler radar was flown on 27 occasions during a series of flight experiments in 1991. Radar calibrations were performed by the flight team to monitor the transmitter power and receiver gain from pre-flight to post-flight and from one day to another. From the recorded calibration data, the receiver gain and effective receiver system noise were calculated and tabulated, together with the transmitter power. These quantities of interest are compared for two receiver/transmitter (R/T) units and two intermediate frequency (IF) bandwidths that were tested in various modes. It was found that, in most operating modes, gain stayed within a 2.5-dB range and transmitter power stayed within a 20-watt range. R/T number 1 had 0.8 dB more gain and 1.2 dBm less noise power than R/T number 2. The 7-MHz IF bandwidth resulted in 1 dB more gain and 1 dBm less noise than the 2-MHz IF bandwidth. Depending on the R/T unit and IF bandwidth, the effective system noise power averaged between -107.3 dBm and -109.5 dBm.
Document ID
19920019633
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Mackenzie, Anne I.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1992
Subject Category
Communications And Radar
Report/Patent Number
NAS 1.15:107589
NASA-TM-107589
Report Number: NAS 1.15:107589
Report Number: NASA-TM-107589
Accession Number
92N28876
Funding Number(s)
PROJECT: RTOP 505-64-12-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available