02078oam 2200613I 450 991071390730332120201211085751.0(CKB)5470000002506594(OCoLC)761203525(EXLCZ)99547000000250659420111115j196903 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierEffects of bottom-structure flexibility on water landing loads of Apollo spacecraft models /by Sandy M. Stubbs and Melvin E. HathawayWashington, D.C. :National Aeronautics and Space Administration,March 1969.1 online resource (30 pages) illustrationsNASA technical note ;NASA TN D-5108"March 1969."Includes bibliographical references (page 11).Space vehiclesLandingImpactShielding (Heat)MaterialsTestingMaterialsDynamic testingImpactfastMaterialsDynamic testingfastShielding (Heat)MaterialsTestingfastSpace vehiclesLandingfastSpace vehiclesLanding.Impact.Shielding (Heat)MaterialsTesting.MaterialsDynamic testing.Impact.MaterialsDynamic testing.Shielding (Heat)MaterialsTesting.Space vehiclesLanding.Stubbs Sandy M.1420794Hathaway Melvin E.United States.National Aeronautics and Space Administration,Langley Research Center.OCLCEOCLCEOCLCQOCLCFOCLCQCOPOCLCOGPOBOOK9910713907303321Effects of bottom-structure flexibility on water landing loads of Apollo spacecraft models3539961UNINA