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A unified acquisition system for acoustic dataA multichannel, acoustic AM carrier system was developed for a wide variety of applications, particularly for aircraft noise and sonic boom measurements. Each data acquisition channel consists of a condenser microphone, an acoustic signal converter, and a Zero Drive amplifier, along with peripheral supporting equipment. A control network insures continuous optimal tuning of the converter and permits remote calibration of the condenser microphone. With a 12.70-mm (1/2-in.) condenser microphone, the converter/Zero Drive amplifier combination has a frequency response from 0 Hz to 20 kHz (-3 db), a dynamic range exceeding 70 db, and a minimum noise floor of 50 db ref. 20 micro Pa) in the band 22.4 Hz to 22.4 kHz. The system requires no external impedance matching networks and is insensitive to cable length, at least up to 900 m (3,000 ft). System gain varies only + or - 1 db over the temperature range 4 to 54 C (40 to 130 F). Adapters are available to accommodate 23.77-mm (1-in.) and 6.35-mm (1/4-in.) microphones and to provide 30-db attenuation. A field test to obtain the acoustical time history of a helicopter flyover proved successful.
Document ID
19770013462
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Zuckerwar, A. J.
(Old Dominion Univ Norfolk, Va., United States)
Holmes, H. K.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
March 1, 1977
Subject Category
Instrumentation And Photography
Report/Patent Number
NASA-TN-D-8327
L-10915
Report Number: NASA-TN-D-8327
Report Number: L-10915
Accession Number
77N20406
Funding Number(s)
PROJECT: RTOP 505-03-11-06
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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