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ANALYSIS OF AERODYNAMIC PHENOMENA ASSOCIATED WITH THE QUARTZ-HERTZ MOTIONOF THE SPACE SHUTTLE ORBITER

Posted on:1988-05-20Degree:M.SType:Thesis
University:The University of Texas at ArlingtonCandidate:BRANNAN, RAYMOND EUGENE, JRFull Text:PDF
GTID:2472390017957374Subject:Aerospace engineering
Abstract/Summary:PDF Full Text Request
This research attempted to use existing shuttle test data to identify causes of the low amplitude roll-yaw oscillation of the space shuttle orbiter during reentry known as quarter-hertz motion. The nature and quantity of the data made any definite conclusions about the direct cause of the motion impossible. Previous theories regarding the quarter-hertz motion were reexamined, taking into consideration as much additional information as possible. Finally, classical control theory was applied to the orbiter system. This indicated that the quarter-hertz is probably a natural lateral-directional response frequency of the system.
Keywords/Search Tags:Shuttle, Motion
PDF Full Text Request
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