Sunday 13th May 2018 Monday 14th May 2018

1 17:0019:0008:3009:00 ROOM10:0010:3012:0012:3015:3018:0019:00 TRADITIONAL DINNER13:45 PRIMES AND OPERATORS VS SUPPLIERS: SPACE TRANSPORTATIONCOFFEE BREAK16:00 PRIMES AND OPERATORS VS SUPPLIERS: SPACECRAFTEND OF DAY 1 WELCOME COFFEEPLENARY SESSION SEVILLACONFERENCE INTRODUCTIONHEAD OF AGENCIES ROUND TABLE: MID AND LONG TERM POLICIESKEYNOTE SPEECH 1 LUNCHREGISTRATIONS unday 13th May 2018 REGISTRATIONWELCOME COCKTAILM onday 14th May 201812345678 SPACECRAFTSPACE TRANSPORTATIONGENERAL INTERESTROOM08:30 Session 1 - ST - ProgrammesSession 2 - ST - Components: Combustion ChambersSession 3 - ST - System ModellingSession 4 - SC - Lessons LearnedSession 5 - SC-CP - Components: Green Monopropellant ThrustersSession 6 - SC-EP - Mission AnalysisSession 7 - SC-EP - Thermal (1)Session 8 - SC - Microsatellite Propulsion (1)ROOMGIRALDATRIANA 1 TRIANA 2 ESPA A 1 ESPA A 2 ESPA A 3 ESPA A 4 ESPA A 5 Chairpersons09:10331 Propulsion systems developments for next generation of the European Vega LauncherE.

2 D'Aversa, Italian Space Agency (ASI), IT270 Characterization of a Multiple Injectors for a Rocket Engine Combustion ChamberG. Jeong, Seoul National University, KR193 Statistical approach in structural mechanics for robust design of liquid rocket enginesC. Marattukalam, ArianeGroup, DE165In-Orbit Performance of the LISA Pathfinder Cold Gas Micro-Propulsion SystemM. George, Airbus Defence & Space, GB388 HAN-based Monopropellant Thruster Development with New Heat-Resistant CatalystH. Keigo, Japan Aerospace Exploration Agency (JAXA), JP529 LiteEPS New Horizons for EP in Constellations DesignD. Lev, Rafael, IL85 Development of a high performance xenon fed resistojetS. Centola, Mars Space Ltd, GB104 Dual Chemical-Electric Propulsion Systems Design for Interplanetary CubeSatsK.

3 V. Mani, Politecnico di Milano, IT09:30328 Development of Rocket Engines in RussiaS. Mosolov, Keldysh Research Center, RU123 Experimental Investigation and Numerical Simulation of Cooling Film in the Nozzle Extension of a LOX/H2 Subscale Thrust ChamberD. Suslov, German Aerospace Center (DLR), DE453 Cycle Analysis and Feasibility Evaluation of Pump fed Hybrid Propulsion SystemR. Hahn, German Aerospace Center (DLR), DE409 Small-GEO Electric Propulsion In-Flight PerformanceS. Beekmans, OHB System, DE134 Development status of a 200mN class low-cost thruster for small Igarashi, IHI Aerospace, JP530 Venus - mission enhancement using electric propulsionD. Lev, Rafael, IL109 Optimum Design of Low Pressure Micro-Resistojets Applied to Nano- and Pico-satellitesD. Cordeiro Guerrieri, TU Delft, NL387 Development and Ground Testing of the PM200 Bi-Propellant CubeSat Propulsion ModuleJ.

4 Wink, Hyperion Technologies, NL09:5072 Getting to Mars and back beyond the initial missionsS. Scimemi, NASA Headquarters, US1763D-printed coaxial injector for a LOX/kerosene rocket engineM. Kuhn, German Aerospace Center (DLR), DE79A presentation of a complete design cycle for optimized hybrid rocket motorsJ. Hijlkema, ONERA, FR147 The 15 years orbital operation summary of DRTS (Data Relay Test Satellite) unified propulsion subsystem and the Lessons and LearnedG. Daisuke, Japan Aerospace Exploration Agency (JAXA), JP549 Development of 1N green propellant thruster in MHI (Mitsubishi Heavy Industries, Ltd.)D. Shiraiwa, Mitsubishi Heavy Industries (MHI), JP465 Mission Scenarios for High-Power Electric PropulsionM. Mammarella, Politecnico di Torino, IT136A GHz Ammonia Microwave Electrothermal Thruster for CubeSats and Small SatellitesM.

5 Micci, Pennsylvania State University, US74 Final Development of the Osaka Institute of Technology 2nd PROITERES Nano-Satellite with High-Power Electrothermal Pulsed Plasma Thrusters for Powered FlightH. Tahara, Osaka Institute of Technology (OIT), JP10:10297 Status of Research Activities on Liquid Rocket Engines in JAXA 2017T. Tomita, Japan Aerospace Exploration Agency (JAXA), JP523 Numerical fatigue life analysis of a prospective LCH4-cooled core stage main combustion chamber wall and comparison to LH2 coolingJ. Riccius, German Aerospace Center (DLR), DE83 Development of fault diagnosis program for liquid rocket engineC. Kim, Korea Aerospace Research Institute (KARI), KR146 The initial orbital operation results of SLATS IES(Ion Engine System) and RCS (reaction Control System)G.

6 Daisuke, Japan Aerospace Exploration Agency (JAXA), JP90 Green Propulsion Advancement and InfusionH. Mulkey, NASA Goddard Space Flight Center, US32 Orbital Maneuvers of Earth Observing Satellites Using Electric Propulsion SystemsM. Kazeev, NRC Kurchatov Insitute, RU160 Design and Flight Qualification of a Micro-Resistojet Payload for the Delfi-PQ SatelliteA. Cervone, Delft University of Technology, NL71 Final Development of Coaxial Pulsed Plasma Thruster systems for Powered Flight onboard the Osaka Institute of Technology 2nd PROITERES Nano-SatelliteK. Enomoto, Osaka Institute of Technology (OIT), JP10:30318 Project Sirius - Affordable Access to Space: Part 1A. Musker, DELTACAT Ltd, GB316 Numerical and Experimental Studies on Pintle Injector for LOX/CH4 EnginesA.

7 Terracciano, Avio, IT170 Implementation of a two-phase pipe component inside the ESPSS libraryF. Pinna, Von Karman Institute for Fluid Dynamics (VKI), BE155 Chemical Propulsion In-flight Experience and Analysis CorrelationI. Fischer, OHB System, DE443 The Experimental Investigation and On-orbit Flying Validation of the ADN-based Liquid ThrusterZ. Yao, Beijing Institute of Control Engineering, CN334 Enhancement of the maneuverability capabilities of a small spacecraft for remote sensing of the earth for stereoscopic surveys based on the unified platform AIST-2I. Tkachenko, Samara University, RU257 High Performance Resistojet Thruster: STAR Status UpdateF. Romei, University of Southampton, GB261 Performance Improvement and Flight Model Design of the Water Resistjet Propulsion System, AQUARIUS for 6U CubeSat: EQUULEUSA.

8 Hattori, The University of Tokyo, JP10:5089On the use of Methane in Rocket Nozzle Cooling Channels Bench scale trialsJ. Fridh, KTH Royal Institute of Technology, SE143 RPA 3: new features for modelling rocket propulsion systemsA. Ponomarenko, RP Software+Engineering, DE434 Primary In-Space Experimental results of the HEP-100MF Thruster On Satellite XY-2Y. Shen, Beijing Institute of Control Engineering, CN563 Investigation of the thermal catalytic thruster on han-based monopropellantD. Goza, EDB Fakel, RU73 Deorbit of Space Debris by Exposure of Plasma Flows Exhausted from Electric Thrusters with PROITERES-4 Nano-SatelliteK. Kajihara, Osaka Institute of Technology (OIT), JP300 Performance Evaluation of 10 W Class Water Resistojet: AQUARIUS for CubeSatsK. Nishii, The University of Tokyo, JP511 ThrustMe a provider of electric space propulsion systems for the next generation satellitesA.

9 Aanesland, ThrustMe, FR11:10 Tuesday 15th May 2018 PLENARY SESSION SEVILLAKEYNOTE SPEECH 2: ARIANE 6 AND VEGA PROGRAMMES STATUSS tefano BIANCHI, Head of Space Transportation Development Programmes, ESACOFFEE BREAKSPACECRAFTSPACE TRANSPORTATIONGENERAL INTERESTS ession 9 - ST - ReusabilitySession 10 - ST - Solid Rocket MotorsSession 11 - ST - Modelling: Multi-Phase FlowsSession 12 - SC-CP - Green propulsionSession 13 - SC-CP - Components: Hydrogen Peroxide ThrustersSession 14 - SC-EP - System Analysis (1)Session 15 - SC-EP - Thermal (2)Session 16 - SC - Microsatellite Propulsion (2)ROOMGIRALDATRIANA 1 TRIANA 2 ESPA A 1 ESPA A 2 ESPA A 3 ESPA A 4 ESPA A 5 Chairpersons11:30348 Prometheus: Precursor of new low-cost rocket Engine FamilyP. Simontacchi, ArianeGroup, FR504 Optimal Design of a First Stage SRM for a Class of VEGA Light VehiclesA.

10 Neri, European Space Agency (ESA), IT222A five equation model for the simulation of the two-phase flow in cryogenic coaxial injectorA. Murrone, ONERA, FR28 Overview of the CNES High Performance Green Monopropellant Project : Requirements, Organization & BreakthroughsN. Pelletier, CNES, FR454 Development of a Flight Type 1N Hydrogen Peroxide ThrusterU. Gotzig, ArianeGroup, DE375 Refinement of Performance and Flexibility Needs for Electric PropulsionB. Wollenhaupt, OHB System, DE326 Environmental and Endurance Testing of the STAR Additively Manufactured ResistojetM. Robinson, University of Southampton, GB258 Performance dependence on the microwave frequency of the miniature water ion thruster and its neutralizerY. Nakagawa, The University of Tokyo, JP11:50406 Callisto - Reusable VTOL launcher first stage demonstratorE.