LEADER 01981oam  2200493I  450 
001 9910707130203321
005 20160510103416.0
035   $a(CKB)5470000002462198
035   $a(OCoLC)703645457
035   $a(EXLCZ)995470000002462198
100   $a20110225j199708    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aRandom vibration and torque tests of fasteners secured with cable, room temperature vulcanized (RTV) rubber, and closed cell foam to support the launch of STS-82 /$fV.H. Yost
210  1$aMSFC, Alabama :$cNational Aeronautics and Space Administration, Marshall Space Flight Center,$dAugust 1997.
215   $a1 online resource (iv, 25 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v108539
300   $aTitle from title screen (viewed May 10, 2016).
300   $a"August 1997."
300   $a"Performing organization: George C. Marshall Space Flight Center, Marshall Space Flight Center, Alabama"--Report documentation page.
517   $aRandom vibration and torque tests of fasteners secured with cable, room temperature vulcanized 
606   $aRandom vibration$2nasat
606   $aVibration tests$2nasat
606   $aTorque$2nasat
606   $aBolts$2nasat
606   $aLocking$2nasat
615  7$aRandom vibration.
615  7$aVibration tests.
615  7$aTorque.
615  7$aBolts.
615  7$aLocking.
700   $aYost$b V. H.$01417696
712 02$aGeorge C. Marshall Space Flight Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bSSM
801  1$bSSM
801  2$bGPO
906   $aBOOK
912   $a9910707130203321
996   $aRandom vibration and torque tests of fasteners secured with cable, room temperature vulcanized (RTV) rubber, and closed cell foam to support the launch of STS-82$93527002
997   $aUNINA