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Passive Accelerometer System Measurements on MIRThe Passive Accelerometer System (PAS) is a simple moving ball accelerometer capable of measuring the small magnitude steady relative acceleration that occurs in a low earth orbit spacecraft due to atmospheric drag and the earth's gravity gradient. The acceleration is measured by recording the average velocity of the spherical ball over a suitable time increment. A modified form of Stokes law is used to convert the average velocity into an acceleration. PAS was used to measure acceleration on the MIR space station and on the first United States Microgravity Laboratory (USML-1). The PAS measurement on MIR revealed remarkably low acceleration levels in the SPEKTR module.
Document ID
19980000737
Acquisition Source
Marshall Space Flight Center
Document Type
Contractor Report (CR)
Authors
Alexander, J. Iwan D.
(Alabama Univ. Huntsville, AL United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1997
Subject Category
Spacecraft Instrumentation
Report/Patent Number
NASA/CR-97-205952
NAS 1.26:205952
Report Number: NASA/CR-97-205952
Report Number: NAS 1.26:205952
Funding Number(s)
CONTRACT_GRANT: NAG8-1223
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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