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Design and development of a Micropound Extended Range Thrust Stand (MERTS)The development and operation of a micropound extended range thrust stand are considered. A cesium ion engine was tested in order to determine the measurement accuracy of the apparatus and to verify the calibration techniques used. The ion engine was tracked to within 5 percent. A check of the thrust stand calibration factor against that of the ion engine calibration factor showed a 4.3 percent difference.
Document ID
19720018140
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Stark, K. W.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
August 6, 2013
Publication Date
January 1, 1972
Publication Information
Publication: Significant Accomplishments in Technol., GSFC, 1970
Subject Category
Instrumentation And Photography
Accession Number
72N25790
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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