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035   $a(OCoLC)1196870748
035   $a(OCoLC)995470000002517035
035   $a(EXLCZ)995470000002517035
100   $a20200922j196812    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aBuckling of an equatorial segment of a spherical shell loaded by its own weight /$fby Robert E. Blum and Harvey G. McComb, Jr
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dDecember 1968.
215   $a1 online resource (28 pages) $cillustrations
225 1 $aNASA/TN ;$vD-4921
300   $a"December 1968."
320   $aIncludes bibliographical references (page 18).
606   $aBuckling$2nasat
606   $aSpherical shells$2nasat
606   $aBuckling (Mechanics)$2fast
606   $aGalerkin methods$2fast
606   $aLunar excursion module$2fast
606   $aShells (Engineering)$2fast
615  7$aBuckling.
615  7$aSpherical shells.
615  7$aBuckling (Mechanics)
615  7$aGalerkin methods.
615  7$aLunar excursion module.
615  7$aShells (Engineering)
700   $aBlum$b Robert E.$0230946
702   $aMcComb$b Harvey G.
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bCOP
801  1$bCOP
801  2$bOCLCF
801  2$bOCLCO
801  2$bGPO
906   $aBOOK
912   $a9910715906403321
996   $aBuckling of an equatorial segment of a spherical shell loaded by its own weight$93436659
997   $aUNINA