Technische Universität Dresden
Institut für Luft- und Raumfahrt
Christian Bach
Marschnerstr. 32
01307 Dresden

Phone: +49 (351) 463-38097
Fax: +49 (351) 463-38125
http://ascension-itn.eu

Publications

Publications Overview

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ESR

Title

Authors

1Health monitoring of reuseable rockets: basics for sensor selectionAndrea Vennitti, Tino Schmiel, Christian Bach, Martin Tajmar
1Health Monitoring for RLVs: Architecture selection and discussionAndrea Vennitti, Tino Schmiel, Christian Bach, Martin Tajmar
   
2Cold-Flow tests on Advanced Nozzle Concepts in subsonic retro-flows: development of test-benchGiuseppe Scarlatella, Jan Sieder‑Katzmann, Florian Roßberg, Felix Weber, Martin Tajmar, Christian Bach
2Advanced nozzle concepts in retro-propulsion applications for reusable launch vehicle recovery: a case studyGiuseppe Scarlatella, Martin Tajmar, Christian Bach
2Design 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
   
3Pre-conceptual staging trade-offs of reusable launch vehiclesGuillermo J. Dominguez Calabuig, Jascha Wilken
3Eco-design of future reusable launchers: insight into their life cycle and atmospheric impactGuillermo J. Dominguez Calabuig, Loïs Miraux, Andrew Ross Wilson, Alberto Sarritzu
3Evaluation of Parametric Cost Estimation in the Preliminary Design Phase of Reusable Launch VehiclesSven Stappert, Jascha Wilken, Guillermo J. Dominguez Calabuig, Martin Sippel
3Environmental sustainability of future proposed space activitiesLoïs Miraux, Andrew Ross Wilson, Guillermo J. Dominguez Calabuig
   
4Combustion Chamber Fatigue Life Analysis for Reusable Liquid Rocket Engines (LREs)Gulczynski, Mateusz T; Riccius, Jörg R.; Waxenegger-Wilfing, Günther; Deeken, Jan C.; Oschwald, Michael
4Reusable Liquid Rocket Engines: Parametric Optimization of Critical Components for Engine Cycle ModelingGulczynski, Mateusz T; Jan C.; Oschwald, Michael
4Parametric 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
4Parametric 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
4Turbine Blades for Reusable Liquid Rocket Engines (LRE) – Numerical Fatigue Life InvestigationGulczynski, Mateusz T. ; Riccius, Jörg; Zametaev, Evgeny; Dos Santos Hahn, Robson Henrique ; Waxenegger-Wilfing, Günther ; Deeken, Jan C. ; Oschwald, Michael
4Combustion Chamber Fatigue Life Analysis for Reusable Liquid Rocket Engines (LREs)Gulczynski, Mateusz T; Riccius, Jörg R.; Waxenegger-Wilfing, Günther; Deeken, Jan C.; Oschwald, Michael
4Numerical Turbine Blade Fatigue Life Analysis for Reusable Liquid Rocket Engines (LREs) ApplicationsGulczynski, 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
4Numerical Fatigue Life Analysis of Combustion Chamber Walls for Future Reusable Liquid Rocket Engines (LREs) ApplicationsGulczynski, Mateusz T. and Riccius, Jörg and Waxenegger-Wilfing, Günther and Deeken, Jan C. and Oschwald, Michael
4LUMEN Evolution for Lunar Lander PropulsionDos Santos Hahn, Robson Henrique and Gulczynski, Mateusz T. and Kurudzija, Eldin and Dresia, Kai and Waxenegger-Wilfing, Günther and Deeken, Jan C.
4Numerical LRE Turbine Blade Fatigue Life Analysis Taking Into Account Partial Admission EffectsRiccius, Jörg, Zametaev, Evgeny and Gulczynski, Mateusz T. and Dos Santos Hahn, Robson Henrique
4RLV applications: challenges and benefits of novel technologies for sustainable main stagesGulczynski, 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
   
 5Conceptual study of technologies enabling novel green expendable upper stages with multi-payload/multi-orbit injection capabilityLily 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
 5Roadmap 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
   
6Advanced nozzle concept trade-off and selection criteria based on launcher mission constraintsFelix Weber, Daniele Bianchi, Francesco Nasuti
   
7Sensibility study for different nozzle configuration on the heat load and aerodynamic behaviour for the THEMIS launcherM. Lantelme, A. Bourgoing, C. Bertorello, P. Tran
7Surrogate 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
7Aerothermodynamic study of the SpaceLinerM. Lantelme
   
8Review Of Regression Rate Enhancement Techniques For Hybrid Rocket EnginesC. Glaser, J. Hijlkema, J.Anthoine
8Evaluation of Regression Rate Enhancing Concepts and Techniques for Hybrid Rocket EnginesC. Glaser, J. Hijlkema, J.Anthoine
8Approximating Idealized Hybrid Rocket Fuel Port Geometries Using StepsC. Glaser, J. Hijlkema, J.Anthoine
8Experimental Investigation of Stepped Fuel Grain Geometries in Hybrid Rocket EnginesC. Glaser, R. Gelain, A. E. M. Bertoldi, J. Hijlkema, P. Hendrick and J. Anthoine
8Experimental regression rate profiles of stepped fuel grains in Hybrid Rocket EnginesC. Glaser, R. Gelain, A. E. M. Bertoldi, Q. Levard, J. Hijlkema, J.-Y. Lestrade P. Hendrick and J. Anthoine
8Influences of steps in hybrid rocket engines:Simulation and validation on simplified geometriesC. Glaser, J. Hijlkema, J.-Y. Lestrade, J.Anthoine
8Hybrid Rocket Engines Optimized by Multi-Stepped Design Approach: Experimental InvestigationC. Glaser, J. Hijlkema, J.-Y. Lestrade, J.Anthoine
8The stepped helix hybrid rocket engineC. 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
9Investigation of additive manufacturing techniques for paraffin-based fuel grainsR. Gelain, A. Hauw, E. Bardotti, P. Hendrick
9Characterization of Magnesium Diboride as an Additive for Paraffin-Based Fuel Hybrid RocketsA. E. De Morais Bertoldi, R. Gelain, P. Hendrick
9Design and Commissioning of the MOUETTE Hybrid Rocket Slab BurnerR. Gelain, F. Angeloni, A. E. De Morais Bertoldi, P. Hendrick
9Characterization of Hybrid Rocket Paraffin-Based FuelsA. E. De Morais Bertoldi, R. Gelain, P. Hendrick
9Conceptual Design of a N2O/Paraffin Hybrid Sounding RocketR. Gelain, P. Hendrick
9Hybrid Rocket Engines as Option to Future Application in Brazilian Space SectorA. E. De Morais Bertoldi, T. B. De Araújo, R. Gelain, L. H. Gouvêa, D. Sakay
9Estimation of Regression Rate from Image Analysis in Hybrid Rocket Slab BurnersR. Gelain, A. Petrarolo, O. Assenmacher, A. E. De Morais Bertoldi, A. Ruttgers, P. Hendrick
9Hybrid Rocket Engines as Option to Future Application in Brazilian Space SectorA. E. De Morais Bertoldi, T. B. De Araújo, R. Gelain, L. H. Gouvêa, D. Sakay
   
10Comparison between a 400N Electric Pump Fed Hydrogen Peroxide/Ethanol Thruster and the MMH/NTO Legacy SystemsLivia Ordonez Valles, Uwe Apel, Martin Tajmar, Peter Weuta
10Green propellants and electric pump feeding system: challenges and opportunities of using these technologies for future kick stagesLivia Ordonez Valles, Lily Blondel-Canepari, Uwe Apel, Angelo Pasini, Martin Tajmar
10Challenges and Opportunities of Green Propellants and Electric Pump Feeding for Future European Kick StagesLivia Ordonez Valles, Lily Blondel-Canepari, Uwe Apel, Angelo Pasini, Martin Tajmar
10LunaNova kick stage: an overview of the system propulsion trade-offsLivia Ordonez Valles, Arturs Jasjukevics, Marco Wolf, Lily Blondel Canepari, Uwe Apel, Martin Tajmar, Angelo Pasini
10Analyzing the potentialities of an electric pump-fed new generation kick stage powered by green propellants: a sensitivity analysis approachLivia Ordonez Valles, Uwe Apel, Angelo Pasini, Martin Tajmar
10Analysis and optimization of a 400N electric pump-fed engine powered by green propellantsLivia Ordonez Valles, Uwe Apel, Martin Tajmar
10Development of an electric pump-fed test bench for green propellant rocket enginesLivia Ordonez Valles, Uwe Apel, Martin Tajmar
   
11Trade-off study of green technologies for upper stage applicationsSarritzu, A., Blondel-Canepari, L., Gelain, R., Hendrick, P., & Pasini, A.
11Assessment of Propulsion System Architectures for Green Propellants-based Orbital StagesSarritzu, A., Lauck, F., Werling, L., & Pasini, A.
11Analytical Hierarchy Process-based trade-off analysis of green and hybrid propulsion technologies for upper stage applicationsSarritzu, A., Blondel-Canepari, L., Gelain, R., Hendrick, P., & Pasini, A.
11Cold-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
   
12Analysis of Space Launch Vehicle FailuresLucía Ayala Fernández, Carsten Wiedemann, Vitali Braun
12Analysis of Space Launch Vehicle Failures and Post-Mission Disposal StatisticsLucía Ayala Fernández, Carsten Wiedemann, Vitali Braun
12Reliability estimation methodology for Liquid Rocket EnginesLucía Ayala Fernández, Carsten Wiedemann, Vitali Braun, Enrico Stoll
12Analysis of Post-Mission Disposal options of Space Launch VehiclesLucía Ayala Fernández, Carsten Wiedemann, Vitali Braun
   
13Guidance, Navigation and Control System Design for Multi-Payload and Multi-Orbit InjectionI. Alforja Ruiz, M. Lavagna
13Mission Analysis, GNC and ATD for Reusable Launch Vehicles within ASCenSIon: Multi-Orbit Multi-Payload Injection, Re-Entry and Safe DisposalAlforja 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.
13Design of the Optimal Trajectory for Multi-Payload Multi-Orbit Injection of an Upper StageAlforja Ruiz, I.;Lavagna, M.
13Analysis of Multi-Orbit Multi-Payload Injection Scenarios for an Upper StageAlforja Ruiz, I.;Lavagna, M.;Bastante, J. C.
   
14Reusable Launch Vehicles Re-Entry: Preliminary Architecture Towards Optimal Guidance and ControlAlice De Oliveira, Michèle Lavagna
14Reusable Launchers Re-entry Controlled Dynamics SimulatorAlice De Oliveira, Michèle Lavagna
14Assessment of Reusable Launch Vehicles Re-entry Dynamics Control Effectiveness with Enchances Aerodynamics ModellingAlice De Oliveira, Michèle Lavagna
14Robust Control Design via Structured H-infinity for the Atmospheric Re-entry of Reusable LaunchersAlice De Oliveira, Michèle Lavagna
14Advanced Guidance Design via Successive Convex Optimization for the 6-DoF Atmospheric Re-entry of Reusable LaunchersAlice De Oliveira, Michèle Lavagna
14Advanced and Robust Guidance & Control System for the Recovery of Reusable LaunchersAlice De Oliveira, Michèle Lavagna
   
15Entry Corridor Analysis for Vertical Landing Reusable Launch VehiclesGuadagnini Jacopo, Bonetti Davide, De Zaiacomo Gabriele
15Aerodynamic coefficients estimation tool for re-entry vehicle missionisationGuadagnini Jacopo, De Zaiacomo Gabriele, Bussler Leonid
 15Multidisciplinary Modeling for Missionisation of Re-entry VehiclesGuadagnini Jacopo, Gabriele De Zaiacomo
 15Multidisciplinary Design Optimization for Missionization of Re-entry Vehicles: Preliminary Mission Design and Mission Capabilities Evaluation of Winged Re-entry Vehicles Case StudyGuadagnini Jacopo, De Zaiacomo Gabriele, Federico Toso
 15Mission Analysis and GNC Missionisation of the
Recovery and Vertical Landing of a Reusable Launch
Vehicle
Guadagnini Jacopo, De Zaiacomo Gabriele

 

last updated on 05/12/2023

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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.

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