02109oam 2200589 450 991071700920332120220218141203.0(CKB)5470000002528118(OCoLC)867072156(OCoLC)995470000002528118(EXLCZ)99547000000252811820140102j199207 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierEffect of temperature and gap opening rate on the resiliency of candidate solid rocket booster O-ring materials /Cynthia L. LachWashington, DC :National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program,July 1992.1 online resource (approximately 18 pages) illustrationsNASA/TP ;3226"July 1992."Includes bibliographical references (page 11).ResiliencenasatElastomersnasatBooster rocket enginesnasatSealing (Technology)MaterialsTestingElastomersTestingRockets (Aeronautics)MaterialsTestingElastomersTestingfastResilience.Elastomers.Booster rocket engines.Sealing (Technology)MaterialsTesting.ElastomersTesting.Rockets (Aeronautics)MaterialsTesting.ElastomersTesting.Lach Cynthia L.1417361United States.National Aeronautics and Space Administration.Scientific and Technical Information Program,OCLCEOCLCEOCLCOOCLCQOCLCFOCLCQGPOOCLCOGPOBOOK9910717009203321Effect of temperature and gap opening rate on the resiliency of candidate solid rocket booster O-ring materials3525468UNINA