LEADER 01869nam  2200541   450 
001 9910705785903321
005 20170613083846.0
035   $a(CKB)5470000002452545
035   $a(OCoLC)989974587
035   $a(EXLCZ)995470000002452545
100   $a20170613j199705    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 14$aThe microgravity vibration isolation mount $ea dynamic model for optimal controller design /$fR. David Hampton [and four others]
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Lewis Research Center,$dMay 1997.
215   $a1 online resource (21 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v107478
300   $a"May 1997."
300   $a"Performing organization: National Aeronautics and Space Administration, Lewis Research Center" Report documentation page.
320   $aIncludes bibliographical reference (pages 20-21).
517   $aMicrogravity vibration isolation mount 
606   $aVibration isolators$2nasat
606   $aControllers$2nasat
606   $aDynamic models$2nasat
606   $aMir space station$2nasat
606   $aMicrogravity$2nasat
606   $aSpace platforms$2nasat
606   $aVibration$2nasat
606   $aActuators$2nasat
615  7$aVibration isolators.
615  7$aControllers.
615  7$aDynamic models.
615  7$aMir space station.
615  7$aMicrogravity.
615  7$aSpace platforms.
615  7$aVibration.
615  7$aActuators.
700   $aHampton$b Roy David$01386543
712 02$aLewis Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910705785903321
996   $aThe microgravity vibration isolation mount$93453726
997   $aUNINA