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1. Model-Based Development of a Library with Standard Functions - for Safety-Critical Flight Control Laws
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... Ensuring Numerical Reproducibility for Model-Based Software Engineering. doi: 10.13009/EUCASS2019-790. [15] Nürnberger, K. 2019. Development of Elementary Mathematics Functions in an Avionics Context. ...
2. Single and Multi-Agent Reinforcement Learning Approach to - Optimize Aircraft Ground Trajectories at Airports
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... https://doi.org/10.13009/EUCASS2019-496. [14] Dancila, R., and Botez, R., “Vertical Flight Profile Optimization for a Cruise Segment with RTA Constraints,” The Aeronautical Journal, Vol. 123, No. 1265, ...
3. Results of Hot-fire Testing of 30kN LOX/Methane - Full-expander Cycle Engine
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... great testing operations and various supports for general affairs. References [1] P.Simontacchi et al., “PROMETHEUS: Precursor of new low-cost rocket engine family”, EUCASS2019-743, Madrid, Spain, 2019. [2] ...
4. Numerical simulation of flight effect on the afterburning - plume exhausting from a solid rocket motor
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... in Solid Rocket Motor Plumes”. In : 8t h European Conference for Aeronautics and Aerospace Sciences. Madrid, Spain, 2019. DOI: 10.13009/EUCASS201979. [27] D. Gueyffier, B. Fromentin-Denoziere, J. Simon, ...
5. KARI’s Additive Rocket Initiative for - Low-Cost and Sustainable Access to Space
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... Space Sciences, EUCASS2019-FP0639, Madrid, Spain, 2019. [12] P. Simontacchi, R. Blasi, E. Edeline, S. Sagnier, N. Ravier, A. Espinosa-Ramos, J. Breteau, and Ph. Altenhoefer, PROMETHEUS: Precursor of New ...
6. Research and Development of the Small LOX/Methane - Propulsion System for an Experimental Reusable Winged
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... actuated valve, ” EUCASS2019-222, Madrid, Spain, 2019 [3] Toru Tsukano et al., “Component tests of a LOX/methane full-expander cycle rocket engine: Singleshaft LOX/methane turbopump, ” EUCASS2019-301, ...
7. Design Loop Process for - Injector Dome of Liquid Rocket Engine
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... Conference for aeronautics and Space Sciences (EUCASS), EUCASS2019-660 [14]Liuzzi, D., Rudnykh, M.; Drigo, D.; Ierardo, Architecture Trade-Off for the VEGA-E upper stage LOX/CH4 engine, 7th EUropean Conference ...
8. Design Loop Process for Cooling Jacket of - Liquid Rocket Engine
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... 8TH European Conference for aeronautics and Space Sciences (EUCASS), EUCASS2019-660 [11]Liuzzi, D., Rudnykh, M.; Drigo, D.; Ierardo, Architecture Trade-Off for the VEGA-E upper stage LOX/CH4 engine, 7th ...
9. PROMETHEUS® tests on T1Bench in Vernon - 10th - EUCASS – 9th CEAS
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... Astronautical Congress, Bremen, Germany, 1-5 October 2018 [5] J. Vila, J. Hassin, Technology acceleration process for the THEMIS low cost and reusable prototype, EUCASS2019-97, 8th European Conference ...
10. Research and Test Activities on Advanced Rocket Propellants at DLR?s Institute of Space Propulsion in Lampoldshausen - Lukas Werling? ?, Dominic Freudenmann? , Sophie C. Ricker? , Marius Wilhelm? , Felix ...
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... Madrid, Spain. doi:10.13009/EUCASS2019-653. [12] M. Negri, F. Lauck, Hot Firing Tests of a Novel Green Hypergolic Propellant in a Thruster, Journal of Propulsion and Power (2022) 1?11doi:10.2514/1.B38413. ...
11. Sustainable Supersonic Transport: a Case Study on Variable Pitot Inlets - Stefan Kazula, Klaus H?schler Brandenburg University of Technology Cottbus-Senftenberg Siemens-Halske-Ring 14, 03046 Cottbus,
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... of Variable Pitot Inlets for Subsonic and Supersonic Business Aviation,? Proceedings of the 8th European Conference for Aeronautics and Space Sciences (Eucass), Madrid, Spain , 2019, doi: 10.13009/EUCASS2019-314. ...
12. Aerothermal characterization of the CALLISTO vehicle during descent - Tobias Ecker? , Moritz Ertl? , Josef Klevanski? , Sven Krummen? and Etienne Dumont? German Aerospace Center (DLR) ? Institute of Aerodynamics ...
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... (EUCASS), Madrid, Spain. July 2019. doi: 10.13009/EUCASS2019-973. [2] E. Dumont, S. Ishimoto, P. Tatiossian, J. Klevanski, B. Reimann, T. Ecker, L. Witte, J. Riehmer, M. Sagliano, S. G. Vincenzino, I. ...
13. Aerothermal analysis of plume interaction with deployed landing legs of the CALLISTO vehicle - Moritz Ertl , Tobias Ecker , Josef Klevanski , Etienne Dumont? and Sven Krummen? German Aerospace Center (DLR) ...
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... and Demonstrators?. In: 8th European Conference for Aeronautics and Space Sciences (EUCASS), Madrid, Spain. July 2019. doi: 10.13009/EUCASS2019-973. E. Dumont, S. Ishimoto, P. Tatiossian, J. Klevanski, ...
14. Configuration Design Studies of a LOX-LCH4 Booster Engine and Stage for a Futuristic Indian Launcher - Kiran Mohan*, Fahd Bin Abdul Hasis**, Vishak Sasidharan, Nandakumar V, Suresh Kumar C and Jayan N ...
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... rocket engine family. DOI: 10.13009/EUCASS2019-743 [5] Sciorelli, F., Jones, M., and Forde, S., ?Collaborative propulsion system analysis tool for pump-fed liquid rocket engines,? Proc. of the 41st AIAA/ASME/SAE/ASEE ...
15. Syntax Warning: PDF version 2.0 -- xpdf supports version 1.7 (continuing anyway) - Reconstruction of the 3D Orientation of a Spinning Sounding Rocket by Detecting the Earth?s Horizon and Sun on Onboard ...
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... Sounding Rocket. In: Proceedings of the 8th European Conference for Aeronautics and Space Sciences. doi: 10.13009/EUCASS2019-241 [3] Braun, B., Barf, J. 2022. Image Processing Based Horizon Sensor for ...
16. Numerical Simulations of the Combustion Process in a Research Thruster operating with N2O/C2H4 and Comparison to Experimental Data - Lukas Werling?? , Ansgar Bachmann? , Nikolaos Perakis? , Torsten Methling? ...
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... and Space Sciences (EUCASS), 1.-4. July 2019, Madrid, Spain. doi:10.13009/EUCASS2019276. URL http://www.eucass2019.eu/ [21] M. Wilhelm, L. Werling, F. Strauss, F. Lauck, C. Kirchberger, H. Ciezki, S. Schlechtriem, ...
17. Development of CMC Combustion Chambers for Advanced Propellants in Space Propulsion - HEIDENREICH, Bernhard* 1, WERLING, Lukas** ?, KURILOV Maxim2, KIRCHBERGER; Christoph, DAUTH, Lucas1, LEHNERT, Tobias, ...
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... and Space Sciences (EUCASS), 1.-4. July 2019, Madrid, Spain. Accessed: Sep. 3 2019. [Online]. Available: http://www.eucass2019.eu/ [40] A. Sarritzu, L. Blondel-Canepari, R. Gelain, P. Hendrick, and A. ...
18. ANALYTICAL MODELING OF CAPILLARY BIPHASIC DEVICES FOR AERONAUTICAL APPLICATIONS - Patricia Serrano and Francisco J. Redondo Airbus Defence and Space - Powerplant and Installations Paseo John Lennon S/N, ...
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DOI: 10.13009/EUCASS2019-3 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) ANALYTICAL MODELING OF CAPILLARY BIPHASIC DEVICES FOR AERONAUTICAL APPLICATIONS Patricia Serrano and Francisco ...
19. A study on effect of transition on High Lift Configuration Aerodynamics - Wang Xun *, Jin Na * *Science and Technology on Space Physics Laboratory, Beijing, 100076
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DOI: 10.13009/EUCASS2019-13 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) A study on effect of transition on High Lift Configuration Aerodynamics Wang Xun *, Jin Na * *Science and ...
20. Flight Test Analysis and Flight Manual Modelling of the Rolling and Braking Resistance over Unpaved Runways - Vinicius Ayello Deo? Airbus Defence and Space Getafe, Madrid vinicius.ayello@airbus.com ?
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DOI: 10.13009/EUCASS2019-20 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS) DOI: 20 Flight Test Analysis and Flight Manual Modelling of the Rolling and Braking Resistance over ...

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