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THE EFFECT OF PROPELLANT SLOSHING ON THE STABILITY OF AN ACCELEROMETER CONTROLLED RIGID SPACE VEHICLEEffect of propellant sloshing on stability of accelerometer controlled rigid space vehicle
Document ID
19630013797
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Bauer, H. F. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1963
Subject Category
Physics, Solid-State
Report/Patent Number
NASA-TN-D-1831
Report Number: NASA-TN-D-1831
Accession Number
63N23677
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ACCELEROMETER
SPACE VEHICLE
PROPELLANT
SLOSHING

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