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University of Utah four-channel pulse-to-pulse commutated SUPER-LOKI rocket meteorological parachutesonde (electronics)The electronics and temperature sensing units of the pulse-to-pulse rocketsonde are described. The sonde is designed for the 2 1/8-inch dart of the SUPER-LOKI meteorological rocket. In flight, the sonde descends by parachute from rocket apogees of about 75 kilometers. As the sonde descends, it transmits air temperature data back to ground radio receiving stations.
Document ID
19760022398
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Atwood, K. W.
(Utah Univ. Salt Lake City, UT, United States)
Soss, D. A.
(Utah Univ. Salt Lake City, UT, United States)
Date Acquired
September 3, 2013
Publication Date
March 1, 1976
Subject Category
Electronics And Electrical Engineering
Report/Patent Number
NASA-CR-141410
UTEC-UA-76-160
Report Number: NASA-CR-141410
Report Number: UTEC-UA-76-160
Accession Number
76N29486
Funding Number(s)
CONTRACT_GRANT: NAS6-2627
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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