LEADER 01064nam a2200253 i 4500 001 991002829329707536 008 070914s2003 it 000 0 ita d 020 $a8851301743 035 $ab13586622-39ule_inst 040 $aSet. Economia$bita 082 04$a658.151 100 1 $aMucelli, Attilio$0382708 245 12$aL'analisi della gestione aziendale :$bcontrollo dei costi, budgeting, reporting e analisi degli scostamenti, activity based management /$cAttilio Mucelli, Patrizia Moretti 260 $aNapoli :$bSistemi editoriali,$c2003 300 $a269 p. ;$c24 cm 440 0$aImpresa ;$v118 650 4$aAziende$xGestione 700 1 $aMoretti, Patrizia$eauthor$4http://id.loc.gov/vocabulary/relators/aut$0618861 907 $a.b13586622$b29-07-10$c14-09-07 912 $a991002829329707536 945 $aLE025 ECO 658.1 MUC01.01$g1$i2025000211742$lle025$n2007$o-$pE20.00$q-$rl$s- $t0$u21$v11$w21$x0$y.i14552115$z14-09-07 996 $aAnalisi della gestione aziendale$91440305 997 $aUNISALENTO 998 $ale025$b14-09-07$cm$da $e-$fita$git $h2$i0 LEADER 02169nam 2200577Ia 450 001 9910700761103321 005 20110802115112.0 035 $a(CKB)5470000002411395 035 $a(OCoLC)744420941 035 $a(EXLCZ)995470000002411395 100 $a20110802d2011 ua 0 101 0 $aeng 135 $aurcn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 14$aThe effects of foam thermal protection system on the damage tolerance characteristics of composite sandwich structures for launch vehicles$b[electronic resource] /$fA.T. Nettles, A.J. Hodge, and J.R. Jackson 210 1$a[Huntsville], Ala. :$cNational Aeronautics and Space Administration, Marshall Space Flight Center,$d[2011] 215 $a1 online resource (vii, 23 pages) $cillustrations 225 1 $aNASA/TP ;$v2011-216457 300 $aTitle from title screen (viewed on Aug. 2, 2011). 300 $a"February 2011." 320 $aIncludes bibliographical references (pages 22-23). 606 $aDamage assessment$2nasat 606 $aLaunch vehicles$2nasat 606 $aThermal protection$2nasat 606 $aSandwich structures$2nasat 606 $aResidual strength$2nasat 606 $aAres 1 launch vehicle$2nasat 606 $aComposite structures$2nasat 606 $aComposite materials$2nasat 606 $aImpact damage$2nasat 615 7$aDamage assessment. 615 7$aLaunch vehicles. 615 7$aThermal protection. 615 7$aSandwich structures. 615 7$aResidual strength. 615 7$aAres 1 launch vehicle. 615 7$aComposite structures. 615 7$aComposite materials. 615 7$aImpact damage. 700 $aNettles$b A. T$g(Alan T.)$01389578 701 $aHodge$b A. J$01403595 701 $aJackson$b J. R$01403596 712 02$aGeorge C. Marshall Space Flight Center. 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910700761103321 996 $aThe effects of foam thermal protection system on the damage tolerance characteristics of composite sandwich structures for launch vehicles$93551009 997 $aUNINA