Jan Deeken
Jan Deeken
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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
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
Studies on electric pump-fed liquid rocket engines for micro-launchers
G Waxenegger-Wilfing, RHS Hahn, J Deeken
Space Propulsion 452, 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
A reinforcement learning approach for transient control of liquid rocket engines
G Waxenegger-Wilfing, K Dresia, JC Deeken, M Oschwald
arXiv preprint arXiv:2006.11108, 2020
Nonlinear control of an expander-bleed rocket engine using reinforcement learning
K Dresia, G Waxenegger-Wilfing, RH Dos Santos Hahn, JC Deeken, ...
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
LUMEN: Engine cycle analysis of an expander-bleed demonstrator engine for test bench operation
J Deeken, G Waxenegger
“L42” technology demonstrator: Operational experience,”
J Sender, DI Suslov, J Deeken, S Gröning, M Oschwald
Space Propulsion 2016, 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
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
Lumen demonstrator-project overview
JC Deeken, G Waxenegger-Wilfing, M Oschwald, S Schlechtriem
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
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
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
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
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
LUMEN Turbopump-Preliminary Design of Supersonic Turbine
RH Dos Santos Hahn, JC Deeken, T Traudt, M Oschwald, S Schlechtriem, ...
32nd International Symposium on Space Technology and Science, 2019
An overview on the turbopump roadmap for the LUMEN demonstrator engine and on the new turbine test facility
T Traudt, G Waxenegger-Wilfing, R dos Santos Hahn, B Wagner, ...
68th International Astronautical Congress, 25-29, 2017
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 (Scopus …, 2021
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