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Space acceleration measurement system triaxial sensor head error budgetThe objective of the Space Acceleration Measurement System (SAMS) is to measure and record the microgravity environment for a given experiment aboard the Space Shuttle. To accomplish this, SAMS uses remote triaxial sensor heads (TSH) that can be mounted directly on or near an experiment. The errors of the TSH are reduced by calibrating it before and after each flight. The associated error budget for the calibration procedure is discussed here.
Document ID
19920015891
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Thomas, John E.
(NASA Lewis Research Center Cleveland, OH, United States)
Peters, Rex B.
(NASA Lewis Research Center Cleveland, OH, United States)
Finley, Brian D.
(Sverdrup Technology, Inc., Brook Park OH., United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1992
Subject Category
Spacecraft Instrumentation
Report/Patent Number
NASA-TM-105300
E-6647
NAS 1.15:105300
Report Number: NASA-TM-105300
Report Number: E-6647
Report Number: NAS 1.15:105300
Accession Number
92N25134
Funding Number(s)
CONTRACT_GRANT: NAS3-24816
CONTRACT_GRANT: NAS3-25266
PROJECT: RTOP 694-03-OH
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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