- 101. GNC Operations for the BepiColombo Mission to Mercury: First In-flight Experience - Christoph Steiger*, Alkan Altay**, Elsa Montagnon*, Frank Budnik*, Massimo Casasco***, Pascal Espeillac****, Susanne ...
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- DOI: 10.13009/EUCASS2019-218 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) GNC Operations for the BepiColombo Mission to Mercury: First In-flight Experience Christoph Steiger*, Alkan ...
- 102. Optimization of allocation of areas for the falling of the worked-off stages boosters of the launch vehicle based on zoning and classification of the existing impact areas of Baikonur cosmodrome - B.T. ...
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- DOI: 10.13009/EUCASS2019-220 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Optimization of allocation of areas for the falling of the worked-off stages boosters of the launch vehicle ...
- 103. Component tests of a LOX/methane full-expander cycle rocket engine: Electrically actuated valve - Hiroya Asakawa*, Masahiro Tanaka**, Takeshi Takaki*** and Kazuhiro Higashi**** *IHI Corporation 900, Fujiki, ...
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- DOI: 10.13009/EUCASS2019-222 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Component tests of a LOX/methane full-expander cycle rocket engine: Electrically actuated valve Hiroya ...
- 104. Component tests of a LOX/methane full-expander cycle rocket engine: Injector and regeneratively cooled combustion chamber - Satoshi Ukai1, Kazuki Sakaki1, Yasuhiro Ishikawa2, Hiroyuki Sakaguchi3, Shinji ...
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- DOI: 10.13009/EUCASS2019-223 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Component tests of a LOX/methane full-expander cycle rocket engine: Injector and regeneratively cooled ...
- 105. Simulating vibrated ?uids and vibroequilibria in the CFVib microgravity experiment - Salgado S?nchez, P.?? , Fern?ndez, J. , Tinao, I.? , Porter, J.? and Bello, A.? E-USOC, Ciencias y Operaciones Aeroespaciales, ...
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- DOI: 10.13009/EUCASS2019-224 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS) Simulating vibrated ?uids and vibroequilibria in the CFVib microgravity experiment Salgado S?nchez, ...
- 106. Investigation of a European Reusable VTVL First Stage Jascha Wilken* and Sven Stappert* * German Aerospace Center (DLR), Institute of Space Systems, Robert-Hooke-Stra?e 7, 28359 Bremen, Germany jascha ...
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- DOI: 10.13009/EUCASS2019-228 8th european conference for aeronautics and space sciences (eucass) Investigation of a European Reusable VTVL First Stage Jascha Wilken* and Sven Stappert* * German Aerospace ...
- 107. Multiphase Baer-Nunziato type models for the simulation of self-pressurizing tanks - M. Gandol? and P. Barbante? Politecnico di Milano, DAER, Via A. La Masa 34, 20156 Milano, Italy ? Politecnico di Milano, ...
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- DOI: 10.13009/EUCASS2019-229 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS) DOI: 229 Multiphase Baer-Nunziato type models for the simulation of self-pressurizing tanks M. Gandol? ...
- 108. The Verifications and Demonstrations of Self-disintegration Fuel Concept for Hybrid Propulsion - Hongsheng Yu*, Ruiqi Shen*?, Yue Tang**, Suhang Chen*, Luigi T. DeLuca***, Wei Zhang*, Yinghua Ye* * Institute ...
- / Doc Indexer /
- DOI: 10.13009/EUCASS2019-230 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) The Verifications and Demonstrations of Self-disintegration Fuel Concept for Hybrid Propulsion Hongsheng ...
- 109. Multipurpose solenoid valve for pneumatic and hydraulic systems of launch vehicles liquid propellant engines - Vasyl Boiko*, Roman Zozulia**, Dmytro Horiachkin*** Firefly Aerospace Ukraine LLC * bvs4760@gmail.com ...
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- DOI: 10.13009/EUCASS2019-231 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Multipurpose solenoid valve for pneumatic and hydraulic systems of launch vehicles liquid propellant engines Vasyl ...
- 110. Optimal guidance for Toss Back concepts of Reusable Launch Vehicles - Elliot Brendel , Bruno H?riss? and Eric Bourgeois DTIS, ONERA, Universit? Paris Saclay F-91123 Palaiseau, France elliot.brendel@onera.fr, ...
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- DOI: 10.13009/EUCASS2019-232 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS) Optimal guidance for Toss Back concepts of Reusable Launch Vehicles Elliot Brendel , Bruno H?riss? ...
- 111. A point of view about the control of a reusable engine cluster - Stephane Colas*, Serge Le Gonidec*, Philippe Saunois**, Martine Ganet**, Antoine R?my*, Vincent Leboeuf* Ariane GROUP *For?t de Vernon BP806 ...
- / Doc Indexer /
- DOI: 10.13009/EUCASS2019-234 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) A point of view about the control of a reusable engine cluster Stephane Colas*, Serge Le Gonidec*, Philippe ...
- 112. Interaction of Energy Discharge and Hypersonic Vehicle - Nadia Kianvashrad and Doyle Knight ? Rutgers University New Brunswick, NJ 08903, USA nadiakianvashrad@gmail.com ? doyleknight@gmail.com ? Corresponding ...
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- DOI: 10.13009/EUCASS2019-235 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS) DOI: ADD DOINUMBER HERE Interaction of Energy Discharge and Hypersonic Vehicle Nadia Kianvashrad and ...
- 113. Mathematical modeling of transient processes during startup of main liquid propellant engine under hot test conditions - Dmytro Koptilyy, Roman Marchan, Sergey Dolgopolov and Olexiy Nikolayev FireFly Aerospace ...
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- DOI: 10.13009/EUCASS2019-236 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Mathematical modeling of transient processes during startup of main liquid propellant engine under hot ...
- 114. 3D printed acoustic igniter of oxygen-kerosene mixtures for aerospace applications - Roman Marchan*, Andrii Oleshchenko**, Samir Vekilov***, Mihaylo Arsenuk**** and Olexander Bobrov***** *Firefly Aerospace ...
- / Doc Indexer /
- DOI: 10.13009/EUCASS2019-238 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) 3D printed acoustic igniter of oxygen-kerosene mixtures for aerospace applications Roman Marchan*, Andrii ...
- 115. The Influence of Meteorological Conditions on the Icing Performance Penalties on a UAV Airfoil - Nicolas Fajt*, Richard Hann* and Thorsten Lutz** *Norwegian University of Science and Technology, 7034 Trondheim, ...
- / Doc Indexer /
- DOI: 10.13009/EUCASS2019-240 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) The Influence of Meteorological Conditions on the Icing Performance Penalties on a UAV Airfoil Nicolas ...
- 116. Integrated Navigation using MEMS-based Inertial, GPS and Sun Vector Measurements aboard the Spin-Stabilized PMWE-1 Sounding Rocket - Benjamin Braun*, Jochen Barf**, Markus Markgraf*** German Aerospace ...
- / Doc Indexer /
- DOI: 10.13009/EUCASS2019-241 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Integrated Navigation using MEMS-based Inertial, GPS and Sun Vector Measurements aboard the Spin-Stabilized ...
- 117. Novel gelled fuels containing nanoparticles as hypergolic bipropellants with HTP - Sophie Ricker1*2, Maxim Kurilov1, Dominic Freudenmann1, Christoph Kirchberger1, Tobias Hertel2, Helmut Ciezki1 and Stefan ...
- / Doc Indexer /
- DOI: 10.13009/EUCASS2019-242 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Novel gelled fuels containing nanoparticles as hypergolic bipropellants with HTP Sophie Ricker1*2, Maxim ...
- 118. Launcher Vehicle Aerothermodynamics and Fairing Separation Altitude E?ects on Payload Temperature - Alessandro Falchi,? Lorenzo Gentile, Edmondo Minisci Aerospace Centre of Excellence, University of S
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- DOI: 10.13009/EUCASS2019-243 7TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS) DOI: ADD DOINUMBER HERE Launcher Vehicle Aerothermodynamics and Fairing Separation Altitude E?ects ...
- 119. Optimization of the base bleed to control trailing edge ?ows in a wide range of Mach numbers - Alejandro Martinez-Cava1? , Eusebio Valero1 , Jorge Saavedra2 , Francisco Lozano2 and Guillermo Paniagua2 ...
- / Doc Indexer /
- DOI: 10.13009/EUCASS2019-244 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS) Optimization of the base bleed to control trailing edge ?ows in a wide range of Mach numbers Alejandro ...
- 120. Effects of Cavities on Pressure Fluctuation Characteristics of Hypersonic Vehicle Wall Plate - Haiyan Li*, Xing Chen**,Hongbo Lu ,Jian Lin, Nong Chen, *China Academy of Aerospace Aerodynamics, 17 Yungang ...
- / Doc Indexer /
- DOI: 10.13009/EUCASS2019-246 Effects of Cavities on Pressure Fluctuation Characteristics of Hypersonic Vehicle Wall Plate Haiyan Li*, Xing Chen**,Hongbo Lu ,Jian Lin, Nong Chen, *China Academy of Aerospace ...