NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Due to the lapse in federal government funding, NASA is not updating this website. We sincerely regret this inconvenience.

Back to Results
The perfectly ideal accelerometerGiven here is a condensed version of the results and conclusions that developed during the Workshop. Upper limits of residual accelerations that can be tolerated during materials processes, presented as acceptable and as desirable limits, are shown. Designs and capabilities of various accelerometers, and their inherent problems, are compared. Results of acceleration measurements on Spacelab flights are summarized, and expected acceleration levels on the Space Station under various conditions are estimated.
Document ID
19910003114
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Stuhlinger, Ernst
(Teledyne Brown Engineering Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1990
Publication Information
Publication: NASA, Marshall Space Flight Center, Measurement and Characterization of the Acceleration Environment on Board the Space Station
Subject Category
Spacecraft Instrumentation
Accession Number
91N12427
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available