Heat transfer prediction for methane in regenerative cooling channels with neural networks G Waxenegger-Wilfing, K Dresia, JC Deeken, M Oschwald Journal of Thermophysics and Heat Transfer 34 (2), 347-357, 2020 | 54 | 2020 |
Numerically efficient fatigue life prediction of rocket combustion chambers using artificial neural networks K Dresia, G Waxenegger-Wilfing, J Riccius, JC Deeken, M Oschwald Proceedings of the 8th European Conference for Aeronautics and Space Sciences, 2019 | 33 | 2019 |
A reinforcement learning approach for transient control of liquid rocket engines G Waxenegger-Wilfing, K Dresia, J Deeken, M Oschwald IEEE Transactions on Aerospace and Electronic Systems 57 (5), 2938-2952, 2021 | 29 | 2021 |
Machine Learning Methods for the Design and Operation of Liquid Rocket Engines--Research Activities at the DLR Institute of Space Propulsion G Waxenegger-Wilfing, K Dresia, J Deeken, M Oschwald arXiv preprint arXiv:2102.07109, 2021 | 28 | 2021 |
Studies on electric pump-fed liquid rocket engines for micro-launchers G Waxenegger-Wilfing, RHS Hahn, J Deeken Space Propulsion 452, 2018 | 28 | 2018 |
Multidisciplinary design optimization of reusable launch vehicles for different propellants and objectives K Dresia, S Jentzsch, G Waxenegger-Wilfing, RD Santos Hahn, J Deeken, ... Journal of Spacecraft and Rockets 58 (4), 1017-1029, 2021 | 26 | 2021 |
Nonlinear control of an expander-bleed rocket engine using reinforcement learning K Dresia, G Waxenegger-Wilfing, RH Dos Santos Hahn, JC Deeken, ... | 21 | 2021 |
Lumen demonstrator-project overview JC Deeken, G Waxenegger-Wilfing, M Oschwald, S Schlechtriem | 21 | 2021 |
“L42” technology demonstrator: Operational experience,” J Sender, DI Suslov, J Deeken, S Gröning, M Oschwald Space Propulsion 2016, 2016 | 13 | 2016 |
Combustion efficiency of a porous injector during throttling of a LOx/H2 combustion chamber J Deeken, D Suslov, O Haidn, S Schlechtriem Progress in Propulsion Physics 2, 251-264, 2011 | 13 | 2011 |
Implications of cycle variants, propellant combinations and operating regimes on fatigue life expectancies of liquid rocket engines G Waxenegger, J Riccius, E Zametaev, J Deeken, J Sand 7th European Conference for Aeronautics and Space Sciences, Milan, Italy, 3-6, 2017 | 12 | 2017 |
LUMEN: Engine cycle analysis of an expander-bleed demonstrator engine for test bench operation J Deeken, G Waxenegger | 11 | 2016 |
Design and testing of a porous injector head for transpiration cooled combustion chambers J Deeken, D Suslov, O Haidn, S Schlechtriem 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and …, 2010 | 11 | 2010 |
RLV applications: challenges and benefits of novel technologies for sustainable main stages MT Gulczynski, A Vennitti, G Scarlatella, GJD Calabuig, ... Proceedings of the International Astronautical Congress, IAC, 2021 | 10 | 2021 |
Liquid Upper Stage Demonstrator Engine (LUMEN): Component Test Results and Project Progress T Traudt, M Börner, D Suslov, RH Dos Santos Hahn, AM Saraf, S Klein, ... | 9 | 2022 |
Utilization of LOX/LCH4 for expander-bleed cycle at upper stage engine application R Hahn, G Waxenegger, J Deeken, M Oschwald, S Schlechtriem EUCASS 2017, 2017 | 9 | 2017 |
Combustion Performance and Stability of a Porous Injector Compared with a State-of-the-Art Coaxial Injector J Deeken, D Suslov, N Rackemann, A Preuss | 9 | 2014 |
LUMEN Thrust Chamber-Injector Design and Stability Analysis J Hardi, JC Deeken, W Armbruster, Y Miene, J Haemisch, J Martin, ... 32nd International Symposium on Space Technology and Science, 2019 | 8 | 2019 |
Determination of the minimum laser pulse energies for ignition in a subscale rocket combustion chamber M Börner, JC Deeken, C Manfletti, M Oschwald Laser ignition conference, LThA4. 2, 2017 | 8 | 2017 |
Combustion efficiency sensitivity studies of the API injector concept J Deeken, D Suslov, O Haidn, S Schlechtriem 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and …, 2011 | 8 | 2011 |