LEADER 01584nam  2200469I  450 
001 9910709891103321
005 20180720131542.0
035   $a(CKB)5470000002473342
035   $a(OCoLC)1045070582
035   $a(EXLCZ)995470000002473342
100   $a20180720j201804    ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aPreload loss in a spacecraft fastener via vibration-induced unwinding /$fChristopher DellaCorte, S. Adam Howard, Daniel P. Hess
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dApril 2018.
215   $a1 online resource (iii, 13 pages) $ccolor illustrations
225 1 $aNASA/TP ;$v2018-219787
300   $a"April 2018."
320   $aIncludes bibliographical references (page 13).
606   $aVibration tests$2nasat
606   $aSlip flow$2nasat
606   $aSolid lubricants$2nasat
606   $aBolted joints$2nasat
606   $aPyrotechnics$2nasat
615  7$aVibration tests.
615  7$aSlip flow.
615  7$aSolid lubricants.
615  7$aBolted joints.
615  7$aPyrotechnics.
700   $aDellaCorte$b Christopher$01386701
702   $aHoward$b S. Adam
702   $aHess$b Daniel P$g(Daniel Peter),
712 02$aNASA Glenn Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910709891103321
996   $aPreload loss in a spacecraft fastener via vibration-induced unwinding$93481513
997   $aUNINA