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Michael Börner
Michael Börner
Institute of Space Propulsion, German Aerospace Center (DLR)
Verified email at dlr.de - Homepage
Title
Cited by
Cited by
Year
Energy loss and charge transfer of argon in a laser-generated carbon plasma
A Frank, A Blažević, V Bagnoud, MM Basko, M Börner, W Cayzac, ...
Physical review letters 110 (11), 115001, 2013
732013
Development of a Nomarski-type multi-frame interferometer as a time and space resolving diagnostics for the free electron density of laser-generated plasma
M Börner, J Fils, A Frank, A Blažević, T Hessling, A Pelka, G Schaumann, ...
Review of Scientific Instruments 83 (4), 2012
312012
Laser ignition of a multi-injector LOX/methane combustor
M Börner, C Manfletti, J Hardi, D Suslov, G Kroupa, M Oschwald
CEAS Space Journal 10 (2), 273-286, 2018
232018
Combustion dynamics in cryogenic rocket engines: Research programme at DLR Lampoldshausen
JS Hardi, T Traudt, C Bombardieri, M Börner, SK Beinke, W Armbruster, ...
Acta Astronautica 147, 251-258, 2018
212018
Laser ignition of an experimental combustion chamber with a multi-injector configuration at low pressure conditions
M Börner, C Manfletti, G Kroupa, M Oschwald
CEAS Space Journal 9 (3), 299-311, 2017
212017
Experimental Study of a Laser-Ignited Liquid Cryogenic Rocket Engine
M Börner, C Manfletti, A Grebe, S Gröning, J Hardi, R Stützer, D Suslov, ...
Laser Ignition Conference 2015, Th2A. 5, 2015
182015
Repetitive laser ignition by optical breakdown of a LOX/H2 rocket combustion chamber with multi-injector head configuration
M Börner, C Manfletti, G Kroupa, M Oschwald
CEAS Space Journal 9 (3), 289-297, 2017
162017
Laser ignition of a multi-injector liquid rocket engine
M Börner, C Manfletti
Space Propulsion Conference, 2014
132014
Injector-coupled thermoacoustic instabilities in an experimental LOX-methane rocket combustor during start-up
S Klein, M Börner, JS Hardi, D Suslov, M Oschwald
CEAS Space Journal, 1-13, 2020
112020
Laser Re-Ignition of a Cryogenic Multi-Injector Rocket Engine
M Börner, C Manfletti, M Oschwald
6TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS), 2015
102015
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, ...
92022
Laser Ignition for Space Propulsion Systems
C Manfletti, M Börner
Laser Ignition Conference 2015, Th2A. 3, 2015
92015
Optical investigation of a laser-ignited cryogenic rocket combustion
R Stützer, M Börner, M Oschwald
6th European Conference for Aeronautics and Space Sciences (EUCASS), 2015
92015
Ignition Overpressure in Laser Ignited Reaction and Control Thrusters
C Manfletti, M Börner
50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 2014
92014
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
82017
A miniaturized high energy laser for ignition of rocket engines
G Kroupa, M Börner
International Conference on Space Optics—ICSO 2018 11180, 1999-2007, 2019
72019
Lumen thrust chamber-flame anchoring for shear coaxial injectors
M Börner, J Martin, J Hardi, D Suslov, JC Deeken, M Oschwald
62021
Laminar burning speeds and flammability limits of CH4/O2 mixtures with varying N2 dilution at sub-atmospheric conditions
A Bee, M Börner
Combustion Science and Technology 195 (8), 1910-1929, 2023
42023
Experimental Study of a Laser Ignited Advanced Porous Injector (API-) Thruster Configuration
M Börner, J Deeken, C Manfletti, M Oschwald
Proceedings, 2016
42016
Methane/oxygen laser ignition in an experimental rocket combustion chamber: impact of mixing and ignition position
M Wohlhüter, V Zhukov, M Börner
Proceedings, 2016
42016
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Articles 1–20