Technische Universität Dresden
Institut für Luft- und Raumfahrt
Christian Bach
Marschnerstr. 32
01307 Dresden
Institut für Luft- und Raumfahrt
Christian Bach
Marschnerstr. 32
01307 Dresden
Phone (): +49 (351) 463-38097
Fax: +49 (351) 463-38125
ascension@tu-dresden.de
http://ascension-itn.eu
Publications
Publications Overview
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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 |
| 1 | Introduction to sensor investigation for RLV health monitoring system | Andrea Vennitti, Tino Schmiel, Christian Bach, Martin Tajmar |
| 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 | 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 |
| 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 |
| 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 | Reusable Liquid Rocket Engines: Parametric Optimization of Critical Components for Engine Cycle Modeling | Gulczynski, Mateusz T; Jan C.; Oschwald, Michael |
| 4 | Parametric Optimization of Turbopump for Reusable Rocket Engine (RRE) Applications | Mateusz T Gulczynski, Robson Henrique Dos Santos Hahn, Günther Waxenegger-Wilfing, Jan C Deeken, Michael Oschwald |
| 4 | Parametric Optimization of Turbopump for Reusable Rocket Engine (RRE) Applications | Mateusz T Gulczynski, Robson Henrique Dos Santos Hahn, Günther Waxenegger-Wilfing, Jan C Deeken, Michael Oschwald |
| 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. and Dos Santos Hahn, Robson Henrique and Riccius, Jörg and Zametaev, Evgeny and Waxenegger-Wilfing, Günther and Deeken, Jan C. and 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 and Gulczynski, Mateusz T. and Kurudzija, Eldin and Dresia, Kai and Waxenegger-Wilfing, Günther and Deeken, Jan C. |
| 4 | Numerical LRE Turbine Blade Fatigue Life Analysis Taking Into Account Partial Admission Effects | Riccius, Jörg, Zametaev, Evgeny and Gulczynski, Mateusz T. and Dos Santos Hahn, Robson Henrique |
| 4 | RLV applications: challenges and benefits of novel technologies for sustainable main stages | Gulczynski, Mateusz T. and Vennitti, Andrea and Scarlatella, Giuseppe and Calabuig, Guillermo Joaquin Dominguez and Blondel-Canepari, Lily and Weber, Felix and Sarritzu, Alberto and Bach, Christian and Deeken, Jan C. and Schmiel, Tino and Bianchi, Daniele and Pasini, Angelo |
| 5 | Conceptual study of technologies enabling novel green expendable upper stages with multi-payload/multi-orbit injection capability | Lily Blondel-Canepari, Inigo Alforja Ruiz, Lucia Ayala Fernandez, Riccardo Gelain, Christopher Glaser, Livia Ordonez Valles, Alberto Sarritzu, Jerome Anthoine, Uwe Apel, Patrick Hendrick, Jouke Hijlkema, Michèle Lavagna, Enrico Stoll, Martin Tajmar, Angelo Pasini |
| 5 | Roadmap Towards a Greener Kick-Stage Propulsion System | Lily Blondel-Canepari, Livia Ordonez Valles, Arturs Jasjukevics, Marco Wolf, Stefane Dussy, Angelo Pasini, Uwe Apel, Martin Tajmar |
| 6 | Advanced nozzle concept trade-off and selection criteria based on launcher mission constraints | Felix Weber, Daniele Bianchi, Francesco Nasuti |
| 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 | Melissa Lantelme, Nathalie Bartoli, Francois Chedevergne, Sylvain Dubreuil, Ysolde Prevereaud |
| 7 | Aerothermodynamic study of the SpaceLiner | M. Lantelme |
| 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 |
| 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 |
| 10 | Comparison between a 400N Electric Pump Fed Hydrogen Peroxide/Ethanol Thruster and the MMH/NTO Legacy Systems | Livia Ordonez Valles, Uwe Apel, Martin Tajmar, Peter Weuta |
| 10 | Green propellants and electric pump feeding system: challenges and opportunities of using these technologies for future kick stages | Livia Ordonez Valles, Lily Blondel-Canepari, Uwe Apel, Angelo Pasini, Martin Tajmar |
| 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 |
| 10 | Development of an electric pump-fed test bench for green propellant rocket engines | Livia Ordonez Valles, Uwe Apel, Martin Tajmar |
| 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 |
| 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 |
| 13 | Guidance, Navigation and Control System Design for Multi-Payload and Multi-Orbit Injection | I. Alforja Ruiz, M. Lavagna |
| 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 | 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. |
| 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 |
| 14 | Advanced and Robust Guidance & Control System for the Recovery of Reusable Launchers | Alice De Oliveira, Michèle Lavagna |
| 15 | Entry Corridor Analysis for Vertical Landing Reusable Launch Vehicles | Guadagnini Jacopo, Bonetti Davide, De Zaiacomo Gabriele |
| 15 | Aerodynamic coefficients estimation tool for re-entry vehicle missionisation | Guadagnini Jacopo, De Zaiacomo Gabriele, Bussler Leonid |
| 15 | Multidisciplinary Modeling for Missionisation of Re-entry Vehicles | Guadagnini Jacopo, Gabriele 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 | Guadagnini Jacopo, De Zaiacomo Gabriele, Federico Toso |
| 15 | Mission Analysis and GNC Missionisation of the Recovery and Vertical Landing of a Reusable Launch Vehicle | Guadagnini Jacopo, De Zaiacomo Gabriele |
last updated on 16/04/2024
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.
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Institut für Luft- und Raumfahrt, Marschnerstr. 32, 01307 Dresden
Quelle: https://ascension-itn.eu/Publications
