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Results of the Advanced Space Structures Technology Research Experiments (ASTREX) hardware and control developmentFuture DOD, NASA, and SDI space systems will be larger than any spacecraft flown before. The economics of placing these Precision Space Systems (PSS) into orbit dictates that they be as low in mass as possible. This stringent weight reduction creates structural flexibility causing severe technical problems when combined with the precise shape and pointing requirements associated with many future PSS missions. Development of new Control Structure Interaction (CSI) technologies which can solve these problems and enable future space missions is being conducted at the Phillips Laboratory, On-Location Site, CA.
Document ID
19930009655
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Cossey, Derek F.
(Phillips Lab. Edwards AFB, CA, United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1993
Publication Information
Publication: NASA. Langley Research Center, The Fifth NASA(DOD Controls-Structures Interaction Technology Conference, Part 1
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
93N18844
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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