LEADER 00986nam0-2200301---450- 001 990009557510403321 005 20120417101035.0 035 $a000955751 035 $aFED01000955751 035 $a(Aleph)000955751FED01 035 $a000955751 100 $a20120417d--------km-y0itay50------ba 101 0 $ager 102 $aDE 105 $a--------001yy 200 1 $aBilanzierung von Optionsanleihen im Handelsrecht$fWalter Busse von Colbe- Bernhard Grossfel- Karl Ludwig Kley (a cura di) 210 $aHidelberg$cR. v. Decker & C.F. Muller$d1987 215 $aX, 177 p.$d25 cm 225 1 $aHamburger Beitrage zum Hnadels-, Schiffahrts- und Wirtschaftsrecht 700 1$aBusse von Colbe,$bWalther$0111665 701 1$aGrossfeld,$bBernhard$0113829 801 0$aIT$bUNINA$gRICA$2UNIMARC 901 $aBK 912 $a990009557510403321 952 $aDPR 21-967$b5227$fDEC 959 $aDEC 996 $aBilanzierung von Optionsanleihen im Handelsrecht$9853757 997 $aUNINA LEADER 02336nam 2200517 450 001 9910706590803321 005 20171114105131.0 035 $a(CKB)5470000002456535 035 $a(OCoLC)1011356298 035 $a(EXLCZ)995470000002456535 100 $a20171113j200102 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aSupersonic wind tunnel tests of a half-axisymmetric 12°-spike inlet to a rocket-based combined-cycle propulsion system /$fJ.R. DeBonis and C.J. Trefny 210 1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dFebruary 2001. 215 $a1 online resource (18 pages) $cillustrations 225 1 $aNASA/TM ;$v2001-210567 300 $a"February 2001." 300 $a"Prepared for the 37th Combustion Subcommittee, 25th Airbreathing Propulsion Subcommittee, and 19th Propulsion Systems Hazards Subcommittee Joint Meeting sponsored by the Joint Army-Navy-Air Force Interagency Propulsion Committee, Monterey, California, November 13-17, 2000." 300 $a"Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field"--Report documentation page. 320 $aIncludes bibliographical references (page 5). 517 3 $aSupersonic wind tunnel tests of a half-axisymmetric 12 degree spike inlet to a rocket-based combined-cycle propulsion system 606 $aAir breathing boosters$2nasat 606 $aHypersonic speed$2nasat 606 $aComputational fluid dynamics$2nasat 606 $aWind tunnel tests$2nasat 606 $aPropulsion$2nasat 606 $aPressure distribution$2nasat 615 7$aAir breathing boosters. 615 7$aHypersonic speed. 615 7$aComputational fluid dynamics. 615 7$aWind tunnel tests. 615 7$aPropulsion. 615 7$aPressure distribution. 700 $aDeBonis$b James R.$01387413 702 $aTrefny$b Charles J. 712 02$aNASA Glenn Research Center, 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910706590803321 996 $aSupersonic wind tunnel tests of a half-axisymmetric 12°-spike inlet to a rocket-based combined-cycle propulsion system$93444583 997 $aUNINA