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035   $a(EXLCZ)995470000002506865
100   $a20111121j196811    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aVibration analysis of a 1/40-scale dynamic model of Saturn V--launch-platform--umbilical-tower configuration /$fby Howard M. Adelman and Earl C. Steeves
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dNovember 1968.
215   $a1 online resource (58 pages) $cillustrations
225 1 $aNASA technical note ;$vTN D-4871
300   $a"November 1968."
320   $aIncludes bibliographical references (page 26).
606   $aLaunch complexes (Astronautics)$xVibration$xMeasurement
606   $aSaturn launch vehicles$xTesting
606   $aFinite element method
606   $aMathematical models
606   $aFinite element method$2fast
606   $aMathematical models$2fast
606   $aSaturn launch vehicles$xTesting$2fast
615  0$aLaunch complexes (Astronautics)$xVibration$xMeasurement.
615  0$aSaturn launch vehicles$xTesting.
615  0$aFinite element method.
615  0$aMathematical models.
615  7$aFinite element method.
615  7$aMathematical models.
615  7$aSaturn launch vehicles$xTesting.
700   $aAdelman$b Howard M.$01400474
702   $aSteeves$b Earl C.
712 02$aUnited States.$bNational Aeronautics and Space Administration,
712 02$aLangley Research Center.
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCO
801  2$bOCLCQ
801  2$bOCLCF
801  2$bGPO
906   $aBOOK
912   $a9910714080503321
996   $aVibration analysis of a 1$93467441
997   $aUNINA