LEADER 00756nam0-22002891i-450- 001 990006501540403321 005 20001010 035 $a000650154 035 $aFED01000650154 035 $a(Aleph)000650154FED01 035 $a000650154 100 $a20001010d--------km-y0itay50------ba 101 0 $aita 105 $ay-------001yy 200 1 $aHow Russia is Ruled$fMerle Fainsod 210 $aCambridge$cHarvard University Press$d1957. 215 $aXIV, 576 p.$d22 cm 676 $a320.80947 700 1$aFainsod,$bMerle$0123248 801 0$aIT$bUNINA$gRICA$2UNIMARC 901 $aBK 912 $a990006501540403321 952 $aXIV F 27$b5949$fFSPBC 959 $aFSPBC 996 $aHow Russia is Ruled$9654719 997 $aUNINA DB $aGEN01 LEADER 01720oam 2200469 450 001 9910716995003321 005 20211025133810.0 035 $a(CKB)5470000002526242 035 $a(OCoLC)1154320734 035 $a(EXLCZ)995470000002526242 100 $a20200514d1938 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aDischarge characteristics of a simulated unit injection system /$fby Edred T. Marsh 210 1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1938. 215 $a1 online resource (9 pages, 5 unnumbered pages) $cillustrations 225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 676 300 $a"November 1938." 300 $aNo Federal Depository Library Program (FDLP) item number. 320 $aIncludes bibliographical references (page 9). 606 $aInternal combustion engines$xFuel systems$xTesting 606 $aNozzles$xTesting 606 $aInjectors$xTesting 606 $aInternal combustion engines$xFuel systems$xTesting$2fast 615 0$aInternal combustion engines$xFuel systems$xTesting. 615 0$aNozzles$xTesting. 615 0$aInjectors$xTesting. 615 7$aInternal combustion engines$xFuel systems$xTesting. 700 $aMarsh$b E. T.$01388391 712 02$aUnited States.$bNational Advisory Committee for Aeronautics, 801 0$bTRAAL 801 1$bTRAAL 801 2$bOCLCO 801 2$bOCLCF 801 2$bGPO 906 $aBOOK 912 $a9910716995003321 996 $aDischarge characteristics of a simulated unit injection system$93438934 997 $aUNINA