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Windshear radar calibration, 1992 flights: Transmitter power and receiver gain stabilityDuring the 1992 NASA airborne Doppler windshear radar flights, radar calibrations were performed prior to each flight in order to determine transmitter power, receiver gain, and receiver noise power. The calibration results show that the average transmitter power in radar mode 6 was 186 watts, with a standard deviation of 7 watts. The average high power amplifier gain was 9.62 dB. At the wide IF bandwidth setting, the receiver gain was 123.1 dB, while at the narrow IF bandwidth setting, the gain was 121.8 dB. The receiver system noise as seen at the receiver input was -107.0 dBmw using the wide IF bandwidth and -107.9 dBmw using the narrow IF bandwidth. In radar mode 7, the receiver gain was the same as in mode 6. However, the receiver noise in mode 7 was about 2.5 dB less using the wide IF bandwidth and 2.0 dB less using the narrow IF bandwidth. The R/T unit flown in 1992 had also been flown the previous year when it produced comparable results. This technical memorandum was written as a follow-up to NASA TM-107589 (June 1992), which describes similar radar calibrations performed during the 1991 windshear radar flight experiments.
Document ID
19940010667
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
August 1, 1993
Subject Category
Communications And Radar
Report/Patent Number
NAS 1.15:108997
NASA-TM-108997
Report Number: NAS 1.15:108997
Report Number: NASA-TM-108997
Accession Number
94N15140
Funding Number(s)
PROJECT: RTOP 505-64-12-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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