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A capacitive accelerometer suitable for telemetryThe design and development of a miniature 0.635 cm (0.25 in.) diameter capacitive accelerometer for use in free flight wind tunnel telemetry are presented. Instruments with full scale ranges from + or - 1 to + or - 200 g were constructed, calibrated, and used in several wind tunnel telemetry projects. Flat, high frequency response from 0 to 1000 Hz or more was obtained by employing the inherent damping and stiffness in the air film surrounding the diaphragm-type spring that supports the inertial mass of the accelerometer. Design features to achieve minimum off-axis sensitivity and temperature stability are discussed, and the design requirements for use of the transducer with telemetry systems are derived. A transducer capacitance change of 0.16 pF full scale gave excellent resolution and provided a frequency deviation of 0.75 MHz for a 100 MHz FM oscillator. Although the present design of the capacitive accelerometer was optimized by using units of 0.635 cm diameter, construction of experimental accelerometers as small as 0.36 cm (0.14 in.) diameter has demonstrated the feasibility of further miniaturization.
Document ID
19720023810
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Coon, G. W.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
September 1, 1972
Subject Category
Instrumentation And Photography
Report/Patent Number
A-4439
NASA-TM-X-2644
Report Number: A-4439
Report Number: NASA-TM-X-2644
Accession Number
72N31460
Funding Number(s)
PROJECT: RTOP 125-24-07-00-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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