000116712 001__ 116712 000116712 005__ 20230425140953.0 000116712 0247_ $$2ISSN$$a0379-6566 000116712 0247_ $$2ISSN$$a1609-042X 000116712 0247_ $$2HSB$$aalm00045426x 000116712 037__ $$aRWTH-CONV-188184 000116712 041__ $$aEnglish 000116712 1001_ $$0P:(DE-82)030315$$aSchmitz, E.$$b0$$eAuthor 000116712 1112_ $$a12. European Aerospace Conference on Progress in Space Transportation$$cParis$$wFrance 000116712 245__ $$aInvestigation of the flow field of the TSTO concept FSSC-12T at subsonic Mach numbers$$hprint 000116712 260__ $$aParis$$bEuropean Space Agency$$c1999 000116712 29510 $$aProceedings of the 12. European Aerospace Conference on Progress in Space Transportation : Paris, France 1999 000116712 3367_ $$0PUB:(DE-HGF)8$$2PUB:(DE-HGF)$$aContribution to a conference proceedings$$bcontrib$$mcontrib 000116712 3367_ $$033$$2EndNote$$aConference Paper 000116712 3367_ $$2ORCID$$aCONFERENCE_PAPER 000116712 3367_ $$2DataCite$$aOutput Types/Conference Paper 000116712 3367_ $$2DRIVER$$aconferenceObject 000116712 3367_ $$2BibTeX$$aINPROCEEDINGS 000116712 3367_ $$0PUB:(DE-HGF)7$$2PUB:(DE-HGF)$$aContribution to a book 000116712 4900_ $$aSpecial Publications European Space Agency$$vo.Nr. 000116712 7001_ $$0P:(DE-82)IDM02694$$aHenze, Andreas$$b1$$eAuthor$$urwth 000116712 7001_ $$0P:(DE-82)IDM00681$$aSchröder, Wolfgang$$b2$$eAuthor 000116712 909CO $$ooai:publications.rwth-aachen.de:116712$$pVDB 000116712 9201_ $$0I:(DE-82)415110_20140620$$k415110$$lLehrstuhl für Strömungslehre und Aerodynamisches Institut$$x0 000116712 961__ $$c2012-09-21$$x2009-07-30$$z2023-04-05 000116712 970__ $$aalm00045426x 000116712 980__ $$acontrib 000116712 980__ $$aI:(DE-82)415110_20140620 000116712 980__ $$aVDB 000116712 980__ $$aUNRESTRICTED 000116712 980__ $$aConvertedRecord 000116712 980__ $$acontb