LEADER 01775oam  2200493I  450 
001 9910709992903321
005 20180820091824.0
035   $a(CKB)5470000002474333
035   $a(OCoLC)1048896278
035   $a(OCoLC)995470000002474333
035   $a(EXLCZ)995470000002474333
100   $a20180820j198310    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aDevelopment of a simplified procedure for rocket engine thrust chamber life prediction with creep $efinal report /$fM.L. Badlani [and three others]
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Lewis Research Center,$dOctober 1983.
215   $a1 online resource (iii, 90 pages) $cillustrations
225 1 $aNASA/CR ;$v168261
300   $a"October 1983."
300   $a"0DAI-1512-11-83."
320   $aIncludes bibliographical references (page 47).
517   $aDevelopment of a simplified procedure for rocket engine thrust chamber life prediction with creep 
606   $aRocket engines$2nasat
606   $aCreep properties$2nasat
606   $aPressure effects$2nasat
606   $aThrust chambers$2nasat
606   $aFinite element method$2nasat
615  7$aRocket engines.
615  7$aCreep properties.
615  7$aPressure effects.
615  7$aThrust chambers.
615  7$aFinite element method.
700   $aBadlani$b M. L.$01411885
712 02$aLewis Research Center,
801  0$bGPO
801  1$bGPO
801  2$bGPO
906   $aBOOK
912   $a9910709992903321
996   $aDevelopment of a simplified procedure for rocket engine thrust chamber life prediction with creep$93504034
997   $aUNINA