| Record ID | marc_oregon_summit_records/catalog_files/osu_bibs.mrc:1443540239:1509 |
| Source | Oregon Libraries |
| Download Link | /show-records/marc_oregon_summit_records/catalog_files/osu_bibs.mrc:1443540239:1509?format=raw |
LEADER: 01509nam a2200409Ka 4500
001 53041485
003 OCoLC
005 20030917142933.0
008 030917s2002 ohu b f000 0 eng d
035 $a(GPO)99127784
037 $a20020081294$bNASA
040 $aGPO$cGPO$dMvI
049 $aORE1
074 $a0830-D (MF)
086 0 $aNAS 1.15:211712
086 0 $aNAS 1.15:211712
100 1 $aPerkins, Hugh Douglas.
245 10 $aEffects of fuel distribution on detonation tube performance$h[microform] /$cHugh Douglas Perkins.
260 $a[Cleveland, Ohio] :$bNational Aeronautics and Space Administration, Glenn Research Center ;$aHanover, MD :$bAvailable from NASA Center for Aerospace Information,$c[2002]
300 $a1 v.
490 1 $a[NASA technical memorandum] ;$vNASA/TM-2002-211712.
533 $aMicrofiche.$b[Washington, D.C. :$cNational Aeronautics and Space Administration,$d2003?]$e1 microfiche.
500 $aShipping list no.: 2003-0300-M.
500 $a"August 2002."
650 7 $aNavier-Stokes equation.$2nasat.
650 7 $aPulse detonation engines.$2nasat.
650 7 $aFuel combustion.$2nasat.
650 7 $aFuel-air ratio.$2nasat.
650 7 $aDetonation.$2nasat.
650 7 $aDetonable gas mixtures.$2nasat.
710 2 $aNASA Glenn Research Center.
830 0 $aNASA technical memorandum ;$v211712.
907 $a.b2303404x$bvdo $cv
902 $a031111
998 $b1$c031011$dm$ea$fv$g0
937 $aAssessment exclusion record.
945 $lvdonf$e1