LEADER 01090nam a2200277 i 4500 001 991001537119707536 005 20020503122708.0 008 010606s1971 us ||| | eng 020 $a3947141601 035 $ab10234974-39ule_inst 035 $aLE01279674$9ExL 040 $aDip.to Lingue$bita 100 1 $aPell, Eve$0464993 245 10$aColonials and sojourners /$cby Paul Jacobs and Saul Landau ; with Eve Pell 260 $aNew York :$bVintage,$cc1971 300 $axxxv,379 p. ;$c18 cm. 490 0 $aTo serve the Devil ;$v2 500 $aIncludes bibliographical references 700 1 $aLandau, Saul$eauthor$4http://id.loc.gov/vocabulary/relators/aut$0563760 700 1 $aJacobs, Paul$eauthor$4http://id.loc.gov/vocabulary/relators/aut$0485273 907 $a.b10234974$b17-02-17$c27-06-02 912 $a991001537119707536 945 $aLE012 305.097 3 JAC 2$cV. 2$g1$i2012000028296$lle012$o-$pE0.00$q-$rl$s- $t0$u0$v0$w0$x0$y.i10284941$z27-06-02 996 $aColonials and sojourners$91445263 997 $aUNISALENTO 998 $ale012$b01-01-01$cm$da $e-$feng$gus $h0$i1 LEADER 01601oam 2200469 450 001 9910717122203321 005 20220214112426.0 035 $a(CKB)5470000002528997 035 $a(OCoLC)846128595 035 $a(EXLCZ)995470000002528997 100 $a20130602j199801 ua 0 101 0 $aeng 135 $aur||||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aComparison of high aspect ratio cooling channel designs for a rocket combustion chamber with development of an optimized design /$fby Mary F. Wadel 210 1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Lewis Research Center,$dJanuary 1998. 215 $a1 online resource (approximately 78 pages) $cillustrations 225 1 $aNASA/TM ;$v1998-206313 300 $a"January 1998." 320 $aIncludes bibliographical references (pages 67-69). 606 $aRocket engines$2nasat 606 $aAspect ratio$2nasat 606 $aCombustion chambers$2nasat 608 $aAcademic theses.$2fast 615 7$aRocket engines. 615 7$aAspect ratio. 615 7$aCombustion chambers. 700 $aWadel$b Mary F.$01394787 712 02$aLewis Research Center, 801 0$bOCLCE 801 1$bOCLCE 801 2$bOCLCQ 801 2$bOCLCO 801 2$bOCL 801 2$bOCLCQ 801 2$bGPO 906 $aBOOK 912 $a9910717122203321 996 $aComparison of high aspect ratio cooling channel designs for a rocket combustion chamber with development of an optimized design$93452546 997 $aUNINA