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 ...
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, ...
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 ...
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? ...
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 ...
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 ...
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? ...
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 ...
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 ...
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 ...
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 ...
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 ...
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 ...
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 ...
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 ...
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 ...
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 ...
DOI: 10.13009/EUCASS2019-247
8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
Experimental Study on Thermal Decomposition of Several Kerosene Fuels
Donghyun Hwang*, Bom Lee**, and Kyubok ...
DOI: 10.13009/EUCASS2019-248
8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
Derivation of Buckling Knockdown Factors Using The Equivalent Model for Isogrid-Stiffened Cylinders
Han-Il ...
DOI: 10.13009/EUCASS2019-251
8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS) DOI: ADD DOINUMBER HERE
3D Conjugate Heat Transfer Analysis of a 100 kN Class Liquid Rocket Combustion ...