NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Method for evaluating gravity effects in the testing of nutation dampersA method is developed for determining the effect of gravity in the testing of nutation dampers on symmetric single or dual spin satellites. The basic theory is developed and then applied to the partially filled viscous ring damper and the spring-mass-dashpot damper. A comparison with test results for the viscous ring damper is also given.-
Document ID
19750058650
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Alfriend, K. T.
(U.S. Navy, Naval Research Laboratory, Washington D.C., United States)
Date Acquired
August 8, 2013
Publication Date
June 1, 1975
Publication Information
Publication: Journal of Spacecraft and Rockets
Volume: 12
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
75A42722
Funding Number(s)
CONTRACT_GRANT: NGR-33-010-169
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available