LEADER 01306nam 2200337Ia 450 001 996388528803316 005 20220215180701.0 035 $a(CKB)1000000000645236 035 $a(EEBO)2240872063 035 $a(OCoLC)ocm47012390e 035 $a(OCoLC)47012390 035 $a(EXLCZ)991000000000645236 100 $a20010525d1656 uy 0 101 0 $alat 135 $aurbn#|||a|bb| 200 10$aIoan. Despauterii Ninivitæ grammaticæ institutionis lib. VII$b[electronic resource] /$fdocte? & concinne? in compendium redacti: per Sebastianum Duisburgensem. Ad prototypum collati & aucti: in usum studiosæ juventutis. Multo? quam antea castigatiores 210 $aEdinburgi, $cExcudebat, Gideon Lithco.$dAnno Dom. 1656 215 $a[130] p 300 $aImperfect: tightly bound with some loss of print. 300 $aReproduction of original in: University of Glasgow Library. 330 $aeebo-0166 606 $aLatin language$xGrammar 615 0$aLatin language$xGrammar. 700 $aSpauter$b Johannes de$f1460-1520.$0860711 701 $aNovimola$b Sebastianus$f1500?-1579.$01001254 801 0$bEAE 801 1$bEAE 906 $aBOOK 912 $a996388528803316 996 $aIoan. Despauterii Ninivitæ grammaticæ institutionis lib. VII$92339632 997 $aUNISA LEADER 02004nam 2200505 450 001 9910707952903321 005 20170202152915.0 035 $a(CKB)5470000002469039 035 $a(OCoLC)971200058 035 $a(EXLCZ)995470000002469039 100 $a20170202j199302 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aSubsonic Aerodynamic characteristics of a proposed advanced manned launch system orbiter configuration /$fGeorge M. Ware and Charles H. Fox, Jr 210 1$a[Washington, D.C.] :$cNational Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program,$dFebruary 1993. 215 $a1 online resource (27 pages) $cillustrations 225 1 $aNASA technical memorandum ;$v4439 300 $a"February 1993" Report documentation page. 300 $a"Performing organization: NASA Langley Research Center"--Report documentation page. 320 $aIncludes bibliographical references (pages 4-5). 606 $aAngle of attack$2nasat 606 $aDelta wings$2nasat 606 $aReusable launch vehicles$2nasat 606 $aRolling moments$2nasat 606 $aSpace transportation system$2nasat 606 $aYawing moments$2nasat 615 7$aAngle of attack. 615 7$aDelta wings. 615 7$aReusable launch vehicles. 615 7$aRolling moments. 615 7$aSpace transportation system. 615 7$aYawing moments. 700 $aWare$b George M.$01410132 702 $aFox$b Charles H. 712 02$aLangley Research Center. 712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Program, 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910707952903321 996 $aSubsonic Aerodynamic characteristics of a proposed advanced manned launch system orbiter configuration$93514251 997 $aUNINA