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Improved HIRAP flight calibration techniqueA method of removing non-aerodynamic acceleration signals and calibrating the High Resolution Accelerometer Package (HiRAP) has been developed and improved. Twelve HiRAP mission data sets have been analyzed applying the improved in-flight calibration technique. The application of flight calibration factors to the data sets from these missions produced calibrated acceleration levels within +/- 5.7 micro-g of zero during a time in-flight when the acceleration level was known to be less than 1 g. To validate the current in-flight calibration technique, the atmospheric density results, specifically the normal-to-axial density ratios, have been compared with the analysis results obtained with the previous in-flight calibration technique. This comparison shows an improvement (up to 12.4 percent per flight) in the density ratio when the updated in-flight calibration technique is used.
Document ID
19920023868
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Moats, Christina D.
(Lockheed Engineering and Sciences Co. Hampton, VA., United States)
Blanchard, Robert C.
(NASA Langley Research Center Hampton, VA, United States)
Larman, Kevin T.
(Lockheed Engineering and Sciences Co. Hampton, VA., United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1992
Subject Category
Spacecraft Instrumentation
Report/Patent Number
NAS 1.15:107656
NASA-TM-107656
Report Number: NAS 1.15:107656
Report Number: NASA-TM-107656
Accession Number
92N33112
Funding Number(s)
PROJECT: RTOP 506-48-11-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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