LEADER 01715nam  2200469I  450 
001 9910705377403321
005 20140428153423.0
035   $a(CKB)5470000002449600
035   $a(OCoLC)878426734
035   $a(EXLCZ)995470000002449600
100   $a20140428d1988      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aOrbit transfer vehicle engine technology program combustor wall condition monitoring, subtask II, task E.5 /$fprepared by B.L. Szemenyei
210  1$aCanoga Park, Calif. :$cRoclwell International, Rocketdyne Division ;$a[Cleveland, Ohio] :$cNational Aeronautics and Space Administration, Lewis Research Center,$d1988.
215   $a1 online resource (35 pages) $cillustrations
225 1 $aNASA-CR ;$v182275
300   $aTitle from title screen (viewed on Apr. 28, 2014).
300   $a"August 1989."
606   $aCombustion chambers$2nasat
606   $aNondestructive tests$2nasat
606   $aThickness$2nasat
606   $aWalls$2nasat
606   $aWear$2nasat
615  7$aCombustion chambers.
615  7$aNondestructive tests.
615  7$aThickness.
615  7$aWalls.
615  7$aWear.
700   $aSzemenyei$b B. L.$01418118
712 02$aRockwell International.$bRocketdyne Division,
712 02$aLewis Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910705377403321
996   $aOrbit transfer vehicle engine technology program combustor wall condition monitoring, subtask II, task E.5$93528542
997   $aUNINA