1–7 of 7 hits
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    Application of non-toxic propellants for future launch vehicles

    Goetz, A. / Maeding, C. / Brummel, L. et al. | AIAA | 2001

    Characterisation of Main Chamber Injectors for GOX/Kerosene in a Single Element Rocket Combustor

    Soller, Sebastian / Wagner, Robert / Kau, Hans-Peter et al. | AIAA | 2005

    Experimental investigation of transpiration cooled hydrogen-oxygen subscale chambers

    Haeseler, D. / Maeding, C. / Rubinskiy, V. et al. | AIAA | 1998

    Characterisation of Combustion and Heat Transfer using GOX/Kerosene in a Single-Element Rocket Combustor

    Soller, Sebastian / Wagner, Robert / Kirchberger, Charles et al. | AIAA | 2005

    Development of advanced technologies for future cryogenic thrust chamber applications

    Zinner, W. / Haeseler, D. / Maeding, C. et al. | AIAA | 1997

    Combustion Stability Characteristics of Coax-Swirl-Injectors for Oxygen/Kerosene AIAA Paper

    Soller, S. / Wagner, R. / Kau, H. et al. | British Library Conference Proceedings | 2007

    LOX-Kerosene Oxidizer-Rich Gas-Generator and Main Combustion Chamber Subscale Testing

    Haeseler, D. / Maeding, C. / Preclik, D. et al. | British Library Conference Proceedings | 2006