LEADER 01237nam--2200397---450- 001 990000385890203316 005 20051111103242.0 010 $a88-464-2691-6 035 $a0038589 035 $aUSA010038589 035 $a(ALEPH)000038589USA01 035 $a0038589 100 $a20010402d2001----km-y0itay0103----ba 101 0 $aita 102 $aIT 105 $a||||||||001yy 200 1 $aMiseria della neopsichiatria$esul delirio e sulla predisposizione schizofrenica$fLuigi Anepeta$gappendice di Nicola Ghezzani 210 $aMilano$cFranco Angeli$dcopyr. 2001 215 $a187 p.$d14 cm 225 2 $aPsicologia$v164 410 0$12001$aPsicologia$v164 606 $aSchizofrenia 676 $a616.898206 700 1$aANEPETA,$bLuigi$0544193 702 1$aGHEZZANI,$bNicola 801 0$aIT$bsalbc$gISBD 912 $a990000385890203316 951 $aII.3. Coll.53/ 31(VI PS C COLL. 15/164)$b157182 L.M.$cVI PS C COLL.$d00008151 959 $aBK 969 $aUMA 979 $aCHIARA$b40$c20010402$lUSA01$h1221 979 $c20020403$lUSA01$h1646 979 $aPATRY$b90$c20040406$lUSA01$h1627 979 $aCOPAT5$b90$c20051111$lUSA01$h1032 996 $aMiseria della neopsichiatria$9875871 997 $aUNISA LEADER 01661oam 2200481 450 001 9910715048203321 005 20210107074505.0 035 $a(CKB)5470000002507522 035 $a(OCoLC)761196833 035 $a(OCoLC)995470000002507522 035 $a(EXLCZ)995470000002507522 100 $a20111115j196809 uy 0 101 0 $aeng 135 $aur||||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aLoad relief autopilot analysis to minimize launch vehicle peak thrust vector deflection requirements /$fby Leslie L. Scalzott and Fred Teren 210 1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dSeptember 1968. 215 $a1 online resource (ii, 39 pages) $cillustrations 225 1 $aNASA technical note ;$vD-4786 320 $aIncludes bibliographical references (page 39). 606 $aAutomatic pilot (Airplanes) 606 $aAerospace vehicles$2nasat 606 $aLaunch vehicles$2nasat 606 $aAutomatic pilots$2nasat 615 0$aAutomatic pilot (Airplanes) 615 7$aAerospace vehicles. 615 7$aLaunch vehicles. 615 7$aAutomatic pilots. 700 $aScalzott$b Leslie L.$01416786 702 $aTeren$b Fred 712 02$aUnited States.$bNational Aeronautics and Space Administration, 801 0$bOCLCE 801 1$bOCLCE 801 2$bOCLCQ 801 2$bOCLCF 801 2$bOCLCQ 801 2$bGPO 906 $aBOOK 912 $a9910715048203321 996 $aLoad relief autopilot analysis to minimize launch vehicle peak thrust vector deflection requirements$93523334 997 $aUNINA