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Design and flight performance evaluation of the Mariners 6, 7, and 9 short-circuit current, open-circuit voltage transducersThe purpose of the short-circuit voltage transducer is to provide engineering data to aid the evaluation of array performance during flight. The design, fabrication, calibration, and in-flight performance of the transducers onboard the Mariner 6, 7 and 9 spacecrafts are described. No significant differences were observed in the in-flight electrical performance of the three transducers. The transducers did experience significant losses due to coverslides or adhesive darkening, increased surface reflection, or spectral shifts within coverslide assembly. Mariner 6, 7 and 9 transducers showed non-cell current degradations of 3-1/2%, 3%, and 4%, respectively at Mars encounter and 6%, 3%, and 4-12%, respectively at end of mission. Mariner 9 solar Array Test 2 showed 3-12% current degradation while the transducer showed 4-12% degradation.
Document ID
19730015507
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Patterson, R. E.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 2, 2013
Publication Date
April 15, 1973
Subject Category
Electronic Equipment
Report/Patent Number
JPL-TM-33-603
NASA-CR-132250
Report Number: JPL-TM-33-603
Report Number: NASA-CR-132250
Accession Number
73N24234
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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