Zobrazeno 1 - 10
of 19
pro vyhledávání: '"C, Deeken"'
Publikováno v:
International Journal of Energetic Materials and Chemical Propulsion. 17:263-286
Autor:
Eugen Ruckhäberle, Natalia Krawczyk, Tanja Fehm, M Röper, J. Salmen, C Deeken, LM Schneider, Bernadette Jäger
Publikováno v:
Senologie - Zeitschrift für Mammadiagnostik und -therapie.
Autor:
C, Deeken, S, Ray, A, Zihni, D, Thompson, J, Gluckstein, S, Lake, S, Roll, B, Ndungu, B, Njihia, H, Saidi, R, Lorenz, B, Stechemesser, W, Reinpold, U, Dietz, C T, Germer, J, Winstanley, M, Miserez, R, Fitzgibbons, V, Schumpelick, A C, de Beaux, R, Zollinger, B D, Matthews, S, Baalman, P, Frisella, S, Bandyopadhyay, S, Raza, M, Manu, W, Okinyi, M, Macharia, O, Neema
Publikováno v:
Hernia. 19:S63-S67
Publikováno v:
Laser Ignition Conference 2017.
The minimum laser pulse energy for ignition is determined and compared for two injection concepts and ignition locations for CH4/O2 and H2/O2 in a subscale rocket engine combustion chamber. A numerical scheme for the laser energy transfer into gaseou
Autor:
Tanja Fehm, Eugen Ruckhäberle, M Röper, C Deeken, S Meznaric, J Hofmann, J. Salmen, LM Schneider
Publikováno v:
Geburtshilfe und Frauenheilkunde. 76
Zielsetzung: Bislang gibt es wenig Daten uber den Therapie- und Erkrankungsverlauf bei metastasierten Mammakarzinomen (MBC). Als Mitglied des PRAEGNANT-Netzwerkes legen wir erste Ergebnisse zur Behandlungsqualitat von Hormonrezeptor-positivem Mammaka
Autor:
Jürgen Hoffmann, Eugen Ruckhäberle, Tanja Fehm, LM Schneider, M Röper, J. Salmen, C Deeken, S Meznaric
Publikováno v:
Geburtshilfe und Frauenheilkunde. 76
Autor:
M Röper, Jürgen Hoffmann, J. Salmen, LM Schneider, S Meznaric, C Deeken, Tanja Fehm, Eugen Ruckhäberle
Publikováno v:
Geburtshilfe und Frauenheilkunde. 76
Publikováno v:
Progress in Propulsion Physics.
Thepresentpublicationaddressestheactionstakentostabilizethecombustion chamber assembly using a porous injector head described in a former publication and the test campaign during which the success of these measures was demonstrated. The ¦rst part de
A proper design of an injection system for liquid propellant rocket engines (LPRE) has to ensure a homogenous mixture of the injected propellants, which should result in a stable and highly efficient combustion process. In addition to combustion stab
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::c44da34fdb466f709c20ffb68ea9ebed
https://elib.dlr.de/82004/
https://elib.dlr.de/82004/
Publikováno v:
49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition.
Since a few years DLR Lampoldshausen has been engaged in the development of a new injection concept for cryogenic liquid propellant rocket engines. This concept bases on the injection of the liquid oxygen through a large number of simple tubes while