LEADER 00794nam0-22002891i-450-
001 990000302090403321
005 20001010
035   $a000030209
035   $aFED01000030209
035   $a(Aleph)000030209FED01
035   $a000030209
100   $a20001010d--------km-y0itay50------ba
101 0 $aita
105   $ay-------001yy
200 1 $aHydraulic Systems Analysis - An introduction$fJohn Stringer.
210   $aLondon$cMac Millan$d1976
215   $aXIV,173 p., ill., 24 cm
676   $a660
700  1$aStringer,$bJohn$0336104
801  0$aIT$bUNINA$gRICA$2UNIMARC
901   $aBK
912   $a990000302090403321
952   $a04 172-26$bIRC 872/L$fDINCH
959   $aDINCH
996   $aHydraulic Systems Analysis - An introduction$9128635
997   $aUNINA
DB    $aING01

LEADER 01790nam  2200481 a 450 
001 9910701156603321
005 20111128133927.0
035   $a(CKB)5470000002415481
035   $a(OCoLC)763304966
035   $a(EXLCZ)995470000002415481
100   $a20111128d2011      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 00$aEvaluation of aluminum alloy 2050-T84 microstructure and mechanical properties at ambient and cryogenic temperatures$b[electronic resource] /$fRobert A. Hafley ... [and others]
210  1$aHampton, Va. :$cNational Aeronautics and Space Administration, Langley Research Center,$d[2011]
215   $a1 online resource (viii, 70 pages) $cillustrations (chiefly color)
225 1 $aNASA/TM ;$v2011-217163
300   $aTitle from title screen (viewed on Nov. 28, 2011).
300   $a"July 2011."
320   $aIncludes bibliographical references (pages 16-17).
606   $aAluminum alloys$2nasat
606   $aCompression tests$2nasat
606   $aCryogenic temperature$2nasat
606   $aHeavy lift launch vehicles$2nasat
606   $aTensile tests$2nasat
606   $aPropellant tanks$2nasat
615  7$aAluminum alloys.
615  7$aCompression tests.
615  7$aCryogenic temperature.
615  7$aHeavy lift launch vehicles.
615  7$aTensile tests.
615  7$aPropellant tanks.
701   $aHafley$b Robert A$01396787
712 02$aLangley Research Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910701156603321
996   $aEvaluation of aluminum alloy 2050-T84 microstructure and mechanical properties at ambient and cryogenic temperatures$93510435
997   $aUNINA