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100   $a19910912d1583      uy             |
101 0 $aeng
135   $aurbn||||a|bb|
200 14$aThe vale mans table$b[electronic resource]
210   $a[London $cs.n.$d1583]
215   $a1 broadside $cill
300   $a"Herein is taught ... howe to draine moores, & al other wet grounds or bogges ... Also here is annexed the compasse and the seale ... and the computation of yeares from VVilliam the Conqueror."--First 10 lines of text.
300   $aSigned at end: Robertus Payne descripsit.
300   $aTo the reader dated: From Paines End, the 16. of Nouember. 1583.
300   $aImprint suggested by STC (2nd ed.) and NUC pre-1956 imprints.
300   $aImperfect: torn and cropped at bottom with slight loss of print.
300   $aReproduction of original in the Harvard University Library.
330   $aeebo-0062
606   $aDrainage$vEarly works to 1800
607   $aGreat Britain$xKings and rulers
615  0$aDrainage
700   $aPayne$b Robert$ffl. 1589.$01016359
801  0$bEBL
801  1$bEBL
801  2$bWaOLN
906   $aBOOK
912   $a996387116703316
996   $aThe vale mans table$92377747
997   $aUNISA

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100   $a20180720j201804    ua             0
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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