LEADER 00933nam0-22003011i-450 001 990001748170403321 005 20190527155014.0 035 $a000174817 035 $aFED01000174817 035 $a(Aleph)000174817FED01 035 $a000174817 100 $a20030910d1990----km-y0itay50------ba 101 0 $aita 102 $aIT 200 1 $a<>castanicoltura irpina da frutto e la commercializzazione internazionale$fa cura di Alfredo Curto 210 $aAvellino$cCamera di Commercio Industria Artigianato e Agricoltura$d1990 215 $a54 p.$c56 ill.$d24 cm 610 0 $aCastagne 610 0 $aIrpinia 676 $a634.53 702 1$aCurto,$bAlfredo 801 0$aIT$bUNINA$gRICA$2UNIMARC 901 $aBK 912 $a990001748170403321 952 $a60 634.53 CURA 1990$b2708$fFAGBC 959 $aFAGBC 996 $aCastanicoltura irpina da frutto e la commercializzazione internazionale$9365669 997 $aUNINA LEADER 01808nam 2200493I 450 001 9910702739103321 005 20150224160307.0 035 $a(CKB)5470000002430809 035 $a(OCoLC)903963864 035 $a(EXLCZ)995470000002430809 100 $a20150224j201407 ua 0 101 0 $aeng 135 $aurcn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aPreliminary structural sensitivity study of hypersonic inflatable aerodynamic decelerator using probabilistic methods /$fKaren H. Lyle 210 1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dJuly 2014. 215 $a1 online resource (14 pages) $ccolor illustrations 225 1 $aNASA/TM ;$v2014-218290 300 $aTitle from title screen (viewed Feb. 24, 2015). 300 $a"July 2014." 320 $aIncludes bibliographical references (pages 8-9). 606 $aLarge space structures$2nasat 606 $aHypersonics$2nasat 606 $aAerodynamic loads$2nasat 606 $aSpacecraft design$2nasat 606 $aStructural analysis$2nasat 606 $aMathematical models$2nasat 615 7$aLarge space structures. 615 7$aHypersonics. 615 7$aAerodynamic loads. 615 7$aSpacecraft design. 615 7$aStructural analysis. 615 7$aMathematical models. 700 $aLyle$b Karen H.$01394148 712 02$aLangley Research Center, 712 02$aUnited States.$bNational Aeronautics and Space Administration, 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910702739103321 996 $aPreliminary structural sensitivity study of hypersonic inflatable aerodynamic decelerator using probabilistic methods$93451097 997 $aUNINA