ESR | Title | Authors |
| 1 | Health monitoring of reuseable rockets: basics for sensor selection | Andrea Vennitti, Tino Schmiel, Christian Bach, Martin Tajmar |
| 1 | Health Monitoring for RLVs: Architecture selection and discussion | Andrea Vennitti, Tino Schmiel, Christian Bach, Martin Tajmar |
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| 2 | Cold-Flow tests on Advanced Nozzle Concepts in subsonic retro-flows: development of test-bench | Giuseppe Scarlatella, Jan Sieder‑Katzmann, Florian Roßberg, Felix Weber, Martin Tajmar, Christian Bach |
| 2 | Advanced nozzle concepts in retro-propulsion applications for reusable launch vehicle recovery: a case study | Giuseppe Scarlatella, Martin Tajmar, Christian Bach |
| 2 | Cold-Gas Experiments on Advanced Nozzles in Subsonic Counter-Flows | Giuseppe Scarlatella, Theodor Heutling , Jan Sieder-Katzmann , Felix Weber , Marco Portolani ,Marco Garutti , Daniele Bianchi , Andrea Ferrero , Dario G. Pastrone , Martin Tajmar, Christian Bach |
| 2 | Design and Development of a Cold-flow Set-up for Advanced Nozzles in Subsonic Counter-flows | Giuseppe Scarlatella, Jan Sieder‑Katzmann, Florian Roßberg, Felix Weber, Carlos T. Mancera, Daniele Bianchi, Martin Tajmar, Christian Bach |
| 2 | Numerical study of advanced nozzles for retro-propulsion applications and comparison with experimental data | Giuseppe Scarlatella |
| 2 | Assessment of Mission Capabilities of a Reusable Heavy-lift Launch Vehicle Concept with Aerospike Engine | Giuseppe Scarlatella, Jacopo Guadagnini, Leonardo Paniccà, Gabriele de Zaiacomo, Martin Tajmar, Christian Bach, Dario Pastrone |
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| 3 | Pre-conceptual staging trade-offs of reusable launch vehicles | Guillermo J. Dominguez Calabuig, Jascha Wilken |
| 3 | Eco-design of future reusable launchers: insight into their life cycle and atmospheric impact | Guillermo J. Dominguez Calabuig, Loïs Miraux, Andrew Ross Wilson, Alberto Sarritzu |
| 3 | Evaluation of Parametric Cost Estimation in the Preliminary Design Phase of Reusable Launch Vehicles | Sven Stappert, Jascha Wilken, Guillermo J. Dominguez Calabuig, Martin Sippel |
| 3 | Environmental sustainability of future proposed space activities | Loïs Miraux, Andrew Ross Wilson, Guillermo J. Dominguez Calabuig |
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| 4 | Combustion Chamber Fatigue Life Analysis for Reusable Liquid Rocket Engines (LREs) | Gulczynski, Mateusz T; Riccius, Jörg R.; Waxenegger-Wilfing, Günther; Deeken, Jan C.; Oschwald, Michael |
| 4 | RLV applications: challenges and benefits of novel technologies for sustainable main stages | Gulczynski, Mateusz T.; Vennitti, Andrea; Scarlatella, Giuseppe; Dominguez Calabuig, Guillermo J.; Blondel-Canepari, Lily; Weber, Felix; Sarritzu, Alberto; Bach, Christian; Deeken, Jan C.; Schmiel, Tino; Bianchi, Daniele; Pasini, Angelo
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| 4 | Parametric Optimization of Turbopump for Reusable Rocket Engine (RRE) Applications | Gulczynski,Mateusz T.; Dos Santos Hahn, Robson Henrique; Waxenegger-Wilfing, Günther; Deeken, Jan C.; Oschwald, Michael
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| 4 | Turbine Blades for Reusable Liquid Rocket Engines (LRE) – Numerical Fatigue Life Investigation | Gulczynski, Mateusz T.; Riccius, Jörg; Zametaev, Evgeny; Dos Santos Hahn, Robson Henrique; Waxenegger-Wilfing, Günther; Deeken, Jan C. ; Oschwald, Michael |
| 4 | Combustion Chamber Fatigue Life Analysis for Reusable Liquid Rocket Engines (LREs) | Gulczynski, Mateusz T; Riccius, Jörg R.; Waxenegger-Wilfing, Günther; Deeken, Jan C.; Oschwald, Michael |
| 4 | Numerical Turbine Blade Fatigue Life Analysis for Reusable Liquid Rocket Engines (LREs) Applications | Gulczynski, Mateusz T.; Dos Santos Hahn, Robson Henrique; Riccius, Jörg; Zametaev, Evgeny; Waxenegger-Wilfing, Günther; Deeken, Jan C.; Oschwald, Michael |
| 4 | Numerical Fatigue Life Analysis of Combustion Chamber Walls for Future Reusable Liquid Rocket Engines (LREs) Applications | Gulczynski, Mateusz T. and Riccius, Jörg and Waxenegger-Wilfing, Günther and Deeken, Jan C. and Oschwald, Michael |
| 4 | LUMEN Evolution for Lunar Lander Propulsion | Dos Santos Hahn, Robson Henrique; Gulczynski, Mateusz T.; Kurudzija, Eldin; Dresia, Kai; Waxenegger-Wilfing, Günther; Deeken, Jan C. |
| 4 | Numerical LRE Turbine Blade Fatigue Life Analysis Taking Into Account Partial Admission Effects | Riccius, Jörg, Zametaev, Evgeny; Gulczynski, Mateusz T.; Dos Santos Hahn, Robson Henrique |
| 4 | RLV applications: challenges and benefits of novel technologies for sustainable main stages | Gulczynski, Mateusz T.; Vennitti, Andrea; Scarlatella, Giuseppe; Calabuig, Guillermo Joaquin Dominguez; Blondel-Canepari, Lily; Weber, Felix; Sarritzu, Alberto; Bach, Christian; Deeken, Jan C.; Schmiel, Tino; Bianchi, Daniele; Pasini, Angelo |
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| 5 | Conceptual study of technologies enabling novel green expendable upper stages with multi-payload/multi-orbit injection capability | L. Blondel-Canepari, I. Alforja Ruiz, L. Ayala Fernandez, R. Gelain, C. Glaser, L. Ordonez Valles, A. Sarritzu, J. Anthoine, U. Apel, P. Hendrick, J. Hijlkema, M. Lavagna, E. Stoll, M. Tajmar, A. Pasini |
| 5 | Roadmap Towards a Greener Kick-Stage Propulsion System | L. Blondel-Canepari, L. Ordonez Valles, A. Jasjukevics, M. Wolf, S. Dussy, A. Pasini, U. Apel, M. Tajmar |
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| 6 | Advanced nozzle concept trade-off and selection criteria based on launcher mission constraints | Felix Weber, Daniele Bianchi, Francesco Nasuti |
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| 7 | Sensibility study for different nozzle configuration on the heat load and aerodynamic behaviour for the THEMIS launcher | M. Lantelme, A. Bourgoing, C. Bertorello, P. Tran |
| 7 | Surrogate models for the aerothermodynamic wall quantities in hypersonic laminar flow in the continuum regime for reusable launch vehicles | M. Lantelme, N. Bartoli, F. Chedevergne, S. Dubreuil, Y. Prevereaud |
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| 8 | Review Of Regression Rate Enhancement Techniques For Hybrid Rocket Engines | C. Glaser, J. Hijlkema, J.Anthoine |
| 8 | Evaluation of Regression Rate Enhancing Concepts and Techniques for Hybrid Rocket Engines | C. Glaser, J. Hijlkema, J.Anthoine |
| 8 | Approximating Idealized Hybrid Rocket Fuel Port Geometries Using Steps | C. Glaser, J. Hijlkema, J.Anthoine |
| 8 | Experimental Investigation of Stepped Fuel Grain Geometries in Hybrid Rocket Engines | C. Glaser, R. Gelain, A. E. M. Bertoldi, J. Hijlkema, P. Hendrick and J. Anthoine |
| 8 | Experimental regression rate profiles of stepped fuel grains in Hybrid Rocket Engines | C. Glaser, R. Gelain, A. E. M. Bertoldi, Q. Levard, J. Hijlkema, J.-Y. Lestrade P. Hendrick and J. Anthoine |
| 8 | Influences of steps in hybrid rocket engines:Simulation and validation on simplified geometries | C. Glaser, J. Hijlkema, J.-Y. Lestrade, J.Anthoine |
| 8 | Hybrid Rocket Engines Optimized by Multi-Stepped Design Approach: Experimental Investigation | C. Glaser, J. Hijlkema, J.-Y. Lestrade, J.Anthoine |
| 8 | The stepped helix hybrid rocket engine | C. Glaser, J. Hijlkema, J.-Y. Lestrade, J.Anthoine |
| 8 | Bridging the Technology Gap: Strategies for Hybrid Rocket Engines | C. Glaser, J. Hijlkema, J. Anthoine |
| 8 | Interaction of multiple steps in hybrid rocket engines: Experimental investigation | C. Glaser, J. Hijlkema, J.-Y. Lestrade, J. Anthoine |
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| 9 | 3D Printing Techniques for Paraffin-Based Fuel Grains | R. Gelain, A. E. De Morais Bertoldi, A. Hauw, P. Hendrick |
| 9 | Investigation of additive manufacturing techniques for paraffin-based fuel grains | R. Gelain, A. Hauw, E. Bardotti, P. Hendrick |
| 9 | Characterization of Magnesium Diboride as an Additive for Paraffin-Based Fuel Hybrid Rockets | A. E. De Morais Bertoldi, R. Gelain, P. Hendrick |
| 9 | Design and Commissioning of the MOUETTE Hybrid Rocket Slab Burner | R. Gelain, F. Angeloni, A. E. De Morais Bertoldi, P. Hendrick |
| 9 | Characterization of Hybrid Rocket Paraffin-Based Fuels | A. E. De Morais Bertoldi, R. Gelain, P. Hendrick |
| 9 | Conceptual Design of a N2O/Paraffin Hybrid Sounding Rocket | R. Gelain, P. Hendrick |
| 9 | Hybrid Rocket Engines as Option to Future Application in Brazilian Space Sector | A. E. De Morais Bertoldi, T. B. De Araújo, R. Gelain, L. H. Gouvêa, D. Sakay |
| 9 | Estimation of Regression Rate from Image Analysis in Hybrid Rocket Slab Burners | R. Gelain, A. Petrarolo, O. Assenmacher, A. E. De Morais Bertoldi, A. Ruttgers, P. Hendrick |
| 9 | Hybrid Rocket Engines as Option to Future Application in Brazilian Space Sector | A. E. De Morais Bertoldi, T. B. De Araújo, R. Gelain, L. H. Gouvêa, D. Sakay |
| 9 | Optical investigation of paraffin-based fuel combustion in a hybrid rocket slab burner | R. Gelain, B. de Morais, E. Artur, P. Hendrick, M. Lefebvre |
| 9 | Semantic Image Segmentation of Hybrid Rocket Fuel Combustion Data using Convolutional Neural Networks | O. Assenmacher, A. Rüttgers, A. Petrarolo, R. Gelain |
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| 10 | Challenges and Opportunities of Green Propellants and Electric Pump Feeding for Future European Kick Stages | Livia Ordonez Valles, Lily Blondel-Canepari, Uwe Apel, Angelo Pasini, Martin Tajmar |
| 10 | LunaNova kick stage: an overview of the system propulsion trade-offs | Livia Ordonez Valles, Arturs Jasjukevics, Marco Wolf, Lily Blondel Canepari, Uwe Apel, Martin Tajmar, Angelo Pasini |
| 10 | Analyzing the potentialities of an electric pump-fed new generation kick stage powered by green propellants: a sensitivity analysis approach | Livia Ordonez Valles, Uwe Apel, Angelo Pasini, Martin Tajmar |
| 10 | Analysis and optimization of a 400N electric pump-fed engine powered by green propellants | Livia Ordonez Valles, Uwe Apel, Martin Tajmar |
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| 11 | Trade-off study of green technologies for upper stage applications | Sarritzu, A., Blondel-Canepari, L., Gelain, R., Hendrick, P., & Pasini, A. |
| 11 | Assessment of Propulsion System Architectures for Green Propellants-based Orbital Stages | Sarritzu, A., Lauck, F., Werling, L., & Pasini, A. |
| 11 | Analytical Hierarchy Process-based trade-off analysis of green and hybrid propulsion technologies for upper stage applications | Sarritzu, A., Blondel-Canepari, L., Gelain, R., Hendrick, P., & Pasini, A. |
| 11 | Cold-Flow Testing of Various Injector Designs for a Novel Hypergolic and Green Propellant Combination Developed at DLR Lampoldshausen | Alberto Sarritzu, Angelo Pasini, Philip Teuffel, Felix Lauck |
| 11 | Review and perspectives of “Green” Self-Pressurizing Propellants for In-Space Propulsion and their applicability to Orbital Stages | Alberto Sarritzu, Mario Raffaele Pesante, Simone La Luna, Angelo Pasini |
| 11 | Performance comparison of green propulsion systems for future Orbital Transfer Vehicles | Alberto Sarritzu, Angelo Pasini |
| 11 | Experimental investigation of combustion performance of a green hypergolic bipropellant based on hydrogen peroxide | Alberto Sarritzu, Angelo Pasini, Florian Merz, Lukas Werling, Felix Lauck |
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| 12 | Analysis of Space Launch Vehicle Failures | Lucía Ayala Fernández, Carsten Wiedemann, Vitali Braun |
| 12 | Analysis of Space Launch Vehicle Failures and Post-Mission Disposal Statistics | Lucía Ayala Fernández, Carsten Wiedemann, Vitali Braun |
| 12 | Reliability estimation methodology for Liquid Rocket Engines | Lucía Ayala Fernández, Carsten Wiedemann, Vitali Braun, Enrico Stoll |
| 12 | Analysis of Post-Mission Disposal options of Space Launch Vehicles | Lucía Ayala Fernández, Carsten Wiedemann, Vitali Braun |
| 12 | Uncertainty in remaining orbital lifetime estimation after post-mission disposal | Lucía Ayala Fernández, Carsten Wiedemann, Vitali Braun, Stijn Lemmens |
| 12 | Impact of the ballistic coefficient estimation on orbital lifetime predictions of rocket bodies | Lucía Ayala Fernández, Carsten Wiedemann, Vitali Braun, Stijn Lemmens |
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| 13 | Mission Analysis, GNC and ATD for Reusable Launch Vehicles within ASCenSIon: Multi-Orbit Multi-Payload Injection, Re-Entry and Safe Disposal | Alforja Ruiz, I.;Ayala Fernández, L.;De Oliveira, A.;Dominguez Calabuig, G. J.;Guadagnini, J.;Lantelme, M.;Bartoli, N.;Chedevergne, F.;De Zaiacomo, G.;Dubreuil, S.;Lavagna, M.;Prevereaud, Y.;Stoll, E. |
| 13 | Sensitivity Analysis of Propulsion System Parameters on GNC Strategies for Multi-Orbit Deliveries | Alforja Ruiz, I.;Blondel-Canepari L.; Sarritzu, A.; Pasini,A.; Lavagna, M.
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| 13 | Design of the Optimal Trajectory for Multi-Payload Multi-Orbit Injection of an Upper Stage | Alforja Ruiz, I.;Lavagna, M. |
| 13 | Analysis of Multi-Orbit Multi-Payload Injection Scenarios for an Upper Stage | Alforja Ruiz, I.;Lavagna, M.;Bastante, J. C. |
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| 14 | Reusable Launch Vehicles Re-Entry: Preliminary Architecture Towards Optimal Guidance and Control | Alice De Oliveira, Michèle Lavagna |
| 14 | Reusable Launchers Re-entry Controlled Dynamics Simulator | Alice De Oliveira, Michèle Lavagna |
| 14 | Assessment of Reusable Launch Vehicles Re-entry Dynamics Control Effectiveness with Enchances Aerodynamics Modelling | Alice De Oliveira, Michèle Lavagna |
| 14 | Robust Control Design via Structured H-infinity for the Atmospheric Re-entry of Reusable Launchers | Alice De Oliveira, Michèle Lavagna |
| 14 | Advanced Guidance Design via Successive Convex Optimization for the 6-DoF Atmospheric Re-entry of Reusable Launchers | Alice De Oliveira, Michèle Lavagna |
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| 15 | Entry Corridor Analysis for Vertical Landing Reusable Launch Vehicles | J. Guadagnini, D. Bonetti, G. De Zaiacomo
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| 15 | Aerodynamic coefficients estimation tool for re-entry vehicle missionisation | J. Guadagnini, G. De Zaiacomo, L. Bussler |
| 15 | Multidisciplinary Modeling for Missionisation of Re-entry Vehicles | J. Guadagnini, G. De Zaiacomo |
| 15 | Multidisciplinary Design Optimization for Missionization of Re-entry Vehicles: Preliminary Mission Design and Mission Capabilities Evaluation of Winged Re-entry Vehicles Case Study | J. Guadagnini, G. De Zaiacomo, F. Toso |
| 15 | Mission Analysis and GNC Missionisation of the Recovery and Vertical Landing of a Reusable Launch Vehicle | J. Guadagnini, G. De Zaiacomo
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The project leading to this application has received funding from the European Union’s Horizon 2020 research and innovation programme under the Marie Skłodowska-Curie grant agreement No 860956.
