LEADER 00991nam0-22003371i-450- 001 990001349360403321 010 $a3-540-13620-7 035 $a000134936 035 $aFED01000134936 035 $a(Aleph)000134936FED01 035 $a000134936 100 $a20000920d1994----km-y0itay50------ba 101 0 $aeng 200 1 $aConvex analysis and nonlinear geometric elliptic equations$fIlya J. Bakelman 210 $aBerlin$cSpringer-Verlag$dc1994 215 $axxi, 510 p.$d25 cm 610 0 $aEquazioni e sistemi ellittici 610 0 $aGeometria differenziale globale 610 0 $aFunzioni convesse 610 0 $aInsiemi convessi 676 $a515 700 1$aBakel'man,$bIl'ia Iakovlevich$0368310 801 0$aIT$bUNINA$gRICA$2UNIMARC 901 $aBK 912 $a990001349360403321 952 $a122-D-9$b14840$fMA1 959 $aMA1 962 $a00A05 996 $aConvex analysis and nonlinear geometric elliptic equations$9376130 997 $aUNINA DB $aING01 LEADER 02078oam 2200613I 450 001 9910713907303321 005 20201211085751.0 035 $a(CKB)5470000002506594 035 $a(OCoLC)761203525 035 $a(EXLCZ)995470000002506594 100 $a20111115j196903 ua 0 101 0 $aeng 135 $aur||||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aEffects of bottom-structure flexibility on water landing loads of Apollo spacecraft models /$fby Sandy M. Stubbs and Melvin E. Hathaway 210 1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dMarch 1969. 215 $a1 online resource (30 pages) $cillustrations 225 1 $aNASA technical note ;$vNASA TN D-5108 300 $a"March 1969." 320 $aIncludes bibliographical references (page 11). 606 $aSpace vehicles$xLanding 606 $aImpact 606 $aShielding (Heat)$xMaterials$xTesting 606 $aMaterials$xDynamic testing 606 $aImpact$2fast 606 $aMaterials$xDynamic testing$2fast 606 $aShielding (Heat)$xMaterials$xTesting$2fast 606 $aSpace vehicles$xLanding$2fast 615 0$aSpace vehicles$xLanding. 615 0$aImpact. 615 0$aShielding (Heat)$xMaterials$xTesting. 615 0$aMaterials$xDynamic testing. 615 7$aImpact. 615 7$aMaterials$xDynamic testing. 615 7$aShielding (Heat)$xMaterials$xTesting. 615 7$aSpace vehicles$xLanding. 700 $aStubbs$b Sandy M.$01420794 702 $aHathaway$b Melvin E. 712 02$aUnited States.$bNational Aeronautics and Space Administration, 712 02$aLangley Research Center. 801 0$bOCLCE 801 1$bOCLCE 801 2$bOCLCQ 801 2$bOCLCF 801 2$bOCLCQ 801 2$bCOP 801 2$bOCLCO 801 2$bGPO 906 $aBOOK 912 $a9910713907303321 996 $aEffects of bottom-structure flexibility on water landing loads of Apollo spacecraft models$93539961 997 $aUNINA