01999oam 2200577I 450 991071408050332120201105105853.0(CKB)5470000002506865(OCoLC)761755885(EXLCZ)99547000000250686520111121j196811 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierVibration analysis of a 1/40-scale dynamic model of Saturn V--launch-platform--umbilical-tower configuration /by Howard M. Adelman and Earl C. SteevesWashington, D.C. :National Aeronautics and Space Administration,November 1968.1 online resource (58 pages) illustrationsNASA technical note ;TN D-4871"November 1968."Includes bibliographical references (page 26).Launch complexes (Astronautics)VibrationMeasurementSaturn launch vehiclesTestingFinite element methodMathematical modelsFinite element methodfastMathematical modelsfastSaturn launch vehiclesTestingfastLaunch complexes (Astronautics)VibrationMeasurement.Saturn launch vehiclesTesting.Finite element method.Mathematical models.Finite element method.Mathematical models.Saturn launch vehiclesTesting.Adelman Howard M.1400474Steeves Earl C.United States.National Aeronautics and Space Administration,Langley Research Center.OCLCEOCLCEOCLCQOCLCOOCLCQOCLCFGPOBOOK9910714080503321Vibration analysis of a 13467441UNINA