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Items where Subject is "Institute of Space Systems > Space Launcher Systems Analysis"

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Number of items at this level: 352.

A

  Alforja Ruiz, Iñigo and Ayala Fernández, Lucía and De Oliveira, Alice and Dominguez Calabuig, Guillermo Joaquin and Guadagnini, Jacopo and Lantelme, Melissa and Bartoli, Nathalie and Chedevergne, François and de Zaiacomo, Gabriele and Dubreuil, Sylvain and Lavagna, Michèle and Prevereaud, Ysolde and Stoll, Enrico (2021) Mission Analysis, GNC and ATD for Reusable Launch Vehicles within ASCenSIon: multi-orbit multi-payload injection, re-entry and safe disposal. In: Proceedings of the International Astronautical Congress, IAC. 72nd International Astronautical Congress (IAC), 25.-29. Oktober 2021, Dubai, Vereinigte Arabische Emirate. ISSN 0074-1795. Volltext nicht frei. file

B

  Babb, Grace (2022) Structural Design Analysis of a Reusable Launch Vehicle's Wings. Student thesis, Universität Bremen. Volltext nicht online.

  Bauer, Carola and Garbers, Nicole and Sippel, Martin (2013) The SpaceLiner7 - Vehicle and Rescue Capsule. 29th ISTS, 2.-9. Juni 2013, Nagoya, Japan. file

  Bauer, Carola and Koch, Aaron and Minutolo, Francesco and Grenard, Philippe (2013) Engineering model for rocket exhaust plumes verified by CFD results. 29th ISTS, 2.-9. Juni 2013, Nagoya, Japan. file

  Bauer, Carola and Garbers, Nicole and Johannsson, Magni and Lentsch, Aron (2012) Investigations of the SpaceLiner Passenger Capsule and Various Abort Scenarios. Deutscher Luft- und Raumfahrtkongress 2012, 10.-12. Sept. 2012, Berlin, Deutschland. Volltext nicht frei. file

  Bauer, Carola and Schwanekamp, Tobias and Clark, Vanessa and Garbers, Nicole (2014) Passenger Capsule for the SpaceLiner. 63. Deutscher Luft- und Raumfahrtkongress 2014, 16.09-18.09.2014, Augsburg, Deutschland. file

  Bauer, Waldemar and Rickmers, Peter and Kallenbach, Alexander and Stappert, Sven and Schwarz, René and Sagliano, Marco and Häseker, Janis Sebastian and Flock, Andreas K. and Thiele, Thomas and Bierig, Andreas and Windelberg, Jens and Ksenik, Eugen (2017) Upcoming DLR Reusability Flight Experiment. In: Proceedings of the International Astronautical Congress, IAC. Proceedings of the International Astronautical Congress, IAC, 25-29 September 2017, Adelaide, Australia. filefile

  Bauer, Waldemar and Rickmers, Peter and Kallenbach, Alexander and Stappert, Sven and Wartemann, Viola and Merrem, Clemens Hans-Joachim and Schwarz, René and Sagliano, Marco and Grundmann, Jan Thimo and Flock, Andreas K. and Thiele, Thomas and Kiehn, Daniel and Bierig, Andreas and Windelberg, Jens and Ksenik, Eugen and Bruns, Thorben E. and Ruhe, Tobias and Elsaesser, Henning (2019) DLR Reusability Flight Experiment ReFEx. Acta Astronautica, 168, pp. 57-68. Elsevier. doi: 10.1016/j.actaastro.2019.11.034. ISSN 0094-5765. Volltext nicht online.

  Bayrak, Yusuf Mete (2019) Multibody Simulation of the SpaceLiner Cabin Rescue System. Master's, Universität Bremen. Volltext nicht online.

  Becker, Marcel and Kopp, Alexander (2015) Rettungskapsel-Design und Integration für das Hyperschallverkehrsflugzeug SpaceLiner. DLR-Interner Bericht. SART TN-001/2014. Master's. DLR. 79 S. (Unpublished) Volltext nicht online.

  Berger, Michael (2020) Systemanalyse zu Rocket Lab‘s Electron. Project Report. SART TN-010/2020. 65 S. Volltext nicht online.

  Berger, Michael (2021) Systemanalyse des SpaceX-Starships inklusive Untersuchung der Skydiving-Rückkehrmethode. Bachelor's, Hochschule Bremen. Volltext nicht online.

  Bergmann, Kevin (2021) Re-Entry Analyses and Ground Footprint Determination of Generic Satellites using DRAMA and Python. Project Report. SART TN-003/2021. 51 S. Volltext nicht online.

  Bergmann, Kevin and Dietlein, Ingrid Monika and Marquardt, Pascal (2022) EURASTROS ascent trajectory and abort analysis. 9TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS), 27. Juni - 01. Juli 2022, Lille, Frankreich. file

  Bhagat, Mihir R. and Dumont, Etienne (2014) SPACEX FALCON 9 v1.1, FALCON HEAVY REMODELLING; FALCON 9 v1.1 DESCENT TRAJECTORY AND PERFORMANCE OPTIMIZATION. DLR-Interner Bericht. SART TN-020/2014. DLR Bremen. (Unpublished) Volltext nicht online.

  Blanco Arnao, Gonzalo and Bonetti, Davide and Solescu, Alina and Recupero, Cristina and Domínguez Calabuig, Guillermo and Wilken, Jascha and Sippel, Martin and Bussler, Leonid (2021) RESOLVE: Performance Trajectory Architectures for Re-usable Launcher Concept. Project Report. SART-TN-004/2020. 676 S. Volltext nicht online.

  Bonetti, Davide and De Zaiacome, Gabriele and Dietlein, Ingrid Monika and Esser, Burkard and Guidotti, Guiseppe and Fedele, Alberto and Verant, Jean-Luc and Prevereaud, Ysolde and Gambacciani, Giovanni and Bimbi, Giulia and Governale, Guiseppe and Viola, Nicole (2019) European Flexible Heat Shields: Advanced TPS Design and Tests for Future in-Orbit Demonstration. Int. Conference on Flight Vehicles, Aerothermodynamics and Re-entry Missions & Engineering, 30. Sept. - 3. Okt. 2019, Monopoli, Italien. Volltext nicht online.

  Brückner, Andreas (2018) Massenabschätzung von Raketenmotoren auf Komponentenebene. Master's, Universität Bremen. Volltext nicht online.

  Brünig, Lennart and Krummen, Sven (2018) Entwicklung eines Rapid Control Prototyping Algorithmus für Raumfahrzeug-Simulationen auf Basis optimaler Regelung. DLR-Interner Bericht. SART TN-002/2018. Master's. 66 S. Volltext nicht online.

  Bussler, Leonid and Sippel, M. and von Rüden, David (2022) Reference Concept SLB 8 Booster. Project Report. (Unpublished) Volltext nicht online.

  Bussler, Leonid and Sippel, Martin (2017) Comparison of Return Options for Reusable First Stages. In: 21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017. 21st AIAA International Space Planes and Hypersonics Technologies Conference, 6-9 March 2017, Xiamen, China. doi: 10.2514/6.2017-2137. file

  Bussler, Leonid and Sippel, Martin (2017) Preliminary Analysis of Three Stage to Orbit Configurations including Winged Reusable First Stages. Project Report. SART TN-012/2017. 196 S. Volltext nicht online.

  Bussler, Leonid and Sippel, Martin and Kopp, Alexander (2017) DLR Projekt AKIRA: Referenzkonfigurationen AKIRA SL 7-3 Booster Aurora. Project Report. SART TN-010/2017. 86 S. Volltext nicht online.

  Bussler, Leonid and Stappert, Sven and Krause, Stefan and Cain, Sebastian and Strikert, Gordon (2020) Scaled Experiment Scenario Description. Project Report. Deliverable D2.3. Other. European Commission (EC project number 821953). 28 S. file

  Bussler, Leonid and Stappert, Sven and Sippel, Martin and Garbers, Nicole (2017) Callisto Flight Demonstrator Options winged vs. ballistic. Project Report. SART TN-016/2016. 90 S. Volltext nicht online.

  Bussler, Leonid and Stappert, Sven and Wilken, Jascha and Sippel, Martin and Dietlein, Ingrid and Karl, Sebastian and Hantz, Christian (2019) ANALYSIS OF VTVL AND VTHL REUSABLE LAUNCH VEHICLE CONFIGURATIONS. Internationale Konferenz für Flugfahrzeuge, Aerothermodynamik und Wiedereintrittsmissionen und -technik (FAR), 30. Sept. - 03. Okt. 2019, Monopoli, Italien. file

  Bussler, Leonid and Wilken, Jascha and Stappert, Sven and Sippel, Martin and Dietlein, Ingrid Monika and Dumont, Etienne (2018) Assessment of VTVL and VTHL Reusable First Stages. HiSST 2018, 26–29 November 2018, Moskau, Russland. file

  Böhrk, Hannah and Barth, Tarik and Dietlein, Ingrid and Elsäßer, Henning and Eggers, Thino and Eßmann, Olaf and Koch , Aaron and Kopp, Alexander and Reimer, Thomas and Sippel, Martin and Weihs, Hendrik (2010) REX-Free Flyer: Re-Entry to Earth Experiment - Machbarkeitsstudie. DLR-Interner Bericht. DLR-IB 435-2010/35. DLR. 15 S. (Unpublished) Volltext nicht online.

C

  Callsen, Steffen (2021) Analysis of Rocket Lab’s Electron re-entry with a hypersonic inflatable aerodynamic decelerator (Ballute). Project Report. SART TN-009/2021. 33 S. Volltext nicht online.

  Callsen, Steffen (2022) Critical Analysis of Rocket Lab Neutron Launcher and Missions. Project Report. SART TN-004/2022. 47 S. Volltext nicht online.

  Callsen, Steffen and Stappert, Sven and Sippel, Martin (2021) Preliminary Analysis of Winged Reusable First Stages in Two- and Three-Stage to Orbit Configurations (RLVC4 Gas Generator). Project Report. SART TN-004/2021. 70 S. Volltext nicht online.

  Callsen, Steffen and Stappert, Sven and Sippel, Martin (2022) Study on future European winged reusable launchers. In: 9th European Conference For Aeronautics And Space Science, EUCASS 2022. 9th European Conference for Aeronautics and Space Sciences (EUCASS), 27. Juni - 01. Juli 2022, Lille, Frankreich. file

  Callsen, Steffen and Wilken, Jascha and Stappert, Sven and Sippel, Martin (2022) Feasible options for point-to-point passenger transport with rocket propelled reusable launch vehicles. 73rd International Astronautical Congress (IAC), 18.-22. Sep. 2022, Paris, Frankreich. Volltext nicht online.

  Casali, Elena and Bussler, Leonid and Sippel, Martin (2016) INVESTIGATION OF FEASIBLE FLIGHT TRAJECTORIES AND RE-ENTRY ATMOSPHERIC GUIDANCE FOR SPACELINER 7. DLR-Interner Bericht. SART TN-014/2015. Master's. DLR. (Unpublished) Volltext nicht online.

  Clark, Vanessa (2015) Modelling of Propellant Management Systems in Early-Phase Launcher Development. In: European Conference for Aerospace Sciences. 6th EUROPEAN CONFERENCE FOR AEROSPACE SCIENCES, 29 June - 02 July 2015, Krakow, Poland. filefile

  Clark, Vanessa (2015) SART TN-013-2014 Saturn-V Propellant Management Simulation. DLR-Interner Bericht. DLR Institute of Space Systems. (Unpublished) Volltext nicht online.

  Clark, Vanessa and Bauer, Carola and Dumont, Etienne and Sippel, Martin (2014) Critical Analyses Ariane 6 Incremental and Modular PHH. DLR-Forschungsbericht, DLR-Interner Bericht. SART TN-012/2014. DLR Institute of Space Systems. 85 S. (Unpublished) Volltext nicht online.

  Clark, Vanessa and Johannsson, Magni and Martelo, Antonio (2015) Process Chain Development for Iterative, Concurrent Design of Advanced Space Transportation Systems. In: European Conference for Aerospace Sciences. 6th EUROPEAN CONFERENCE FOR AEROSPACE SCIENCES, 28 June - 02 July 2015, Krakow, Poland. filefile

  Clark, Vanessa Jane (2014) Ariane 6 Upper Stage Deorbitation. Other. SART TN-015/2014. Other. DLR. (Unpublished) Volltext nicht online.

  Clark, Vanessa Jane (2015) Deorbitation of Upper Stages dust v1.1. DLR-Interner Bericht. SART TN-026/2014. Other. DLR. (Unpublished) Volltext nicht online.

  Comitini, Dario (2017) Preliminary safety assessment of a two-stage hypersonic space transportation system. Master's, Politecnico Turino. Volltext nicht online.

  Crai, Alexander (2013) Comparison and data analysis of the exhaust plumes of Athena II and Vega. DLR-Interner Bericht. SART TN20-2013. DLR Bremen. (Unpublished) Volltext nicht online.

D

  David, Emmanuelle (2016) Elaboration of Ariane 6 operational concept with a concurrent engineering approach. In: Proceedings of the 67th International Astronautical Congress. International Astronautical Congress 2016, 26.-30. Sept. 2016, Guadalajara, Mexico. ISBN 9781510835825. file

  David, Emmanuelle and Braun, Vitali (2013) RE-ENTRY ANALYSIS COMPARISON WITH DIFFERENT SOLAR ACTIVITY MODELS OF SPENT UPPER STAGE USING ESA’S DRAMA TOOL. 6th IAASS Conference, Mai. 2013, Montreal, Quebec, Canada. file

  David, Emmanuelle and Fisher, Scott (2013) End-of-Life of Upper Stages in Geostationary Transfer Orbit. DLR-Interner Bericht. SART TN008-2013. DLR Bremen. (Unpublished) Volltext nicht online.

  David, Emmanuelle and Johannsson, Magni (2012) Next Generation Launcher-Potential Ariane 5ME and Ariane 6 Common Upper Stage Options. DLR-Interner Bericht. Deutsches Zentrum für Luft- und Raumfahrt. (Unpublished) Volltext nicht online.

  Dietlein, Ingrid (2008) Kickstage for Aldebaran DWS Study October 2008. Project Report. SART-TN-015/2008. DLR Institut für Raumfahrtsysteme. 33 S. (Unpublished) Volltext nicht online.

  Dietlein, Ingrid and Gamgami, Farid and Sippel, Martin (2008) Kritische Nachanalyse des Wiedereintrittsdemonstrators Pre-X. DLR-Interner Bericht, Project Report. Institut für Raumfahrtsysteme. (Unpublished) Volltext nicht online.

  Dietlein, Ingrid and Schwanekamp, Tobias and Kopp, Alexander (2012) Trim requirements and impact on wing design for the high-speed passenger transport concept SpaceLiner. Journal of Aerospace Engineering, 227 (11), pp. 1811-1826. American Society of Civil Engineers. doi: 10.1177/0954410012463666. Volltext nicht online.

  Dietlein, Ingrid (2013) Beschreibung des Programms fubaco (fuel barycenter computation). DLR-Interner Bericht. SART TN22-2013. DLR Bremen. (Unpublished) Volltext nicht online.

  Dietlein, Ingrid (2014) Beschreibung des Programms exact (extended aerodynamics computation tool). DLR-Interner Bericht. SART TN-025/2014. DLR Bremen. (Unpublished) Volltext nicht online.

  Dietlein, Ingrid and Dumont, Etienne and Kopp, Alexander and Ludwig, Carina (2011) Pre-Design of a Modular Launch System with Single Launch Capacity (NGL). DLR-Interner Bericht. SART TN-022/2010. Other. DLR. 88 S. Volltext nicht online.

  Dietlein, Ingrid and Kopp, Alexander (2009) System Analysis for "Sharp Edge" Re-entry Vehicles. 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, 19. Okt. - 22. Okt 2009, Bremen, Deutschland. file

  Dietlein, Ingrid and Romberg, Oliver (2014) Keine Panik vor Ingenieurmathematik! Springer Vieweg. ISBN 978-3834815675. Volltext nicht online.

  Dietlein, Ingrid Monika (2022) How To Become a Rocket Scientist. Rotary Club Sitzung, 19. Juli 2022, Bremen. Deutschland. (Unpublished) Volltext nicht online.

  Dietlein, Ingrid Monika and Garbers, Nicole and Bussler, Leonid and Wilken, Jascha and Trivailo, Olga (2016) LFBB-(Micro)-Launcher. DLR-Interner Bericht. SART TN-018/2015. Other. DLR. (Unpublished) Volltext nicht online.

  Dietlein, Ingrid Monika and Guidotti, Giuseppe and Trovarelli, F. and Pontijas Fuentes, Irene and Rivero Martín, A. and Esser, Burkard and Schleutker, Thorn and Gambacciani, Giovanni and Governale, Giuseppe and Gardi, Roberto and Verant, J.L. and Dauvois, Yann and Prevereaud, Ysolde (2022) Advanced European Re-Entry System Based on Inflatable Heat Shields EFESTO project overview: preliminary IOD mission and system definition. International Astronautical Congress (IAC 2022), 18-22 September 2022, Paris, France. file

  Dietlein, Ingrid Monika and Guidotti, Guiseppe and Pontijas Fuentes, Irene and Trovarelli, Federico and Rivero Martín, Alejandro and Schleutker, Thorn and Callsen, Steffen and Bergmann, Kevin and Julien, Cedric and Dauvois, Yann and Gardi, Roberto and Gambacciani, Giovanni and Governale, Guiseppe (2022) Development of Inflatable Heat Shield Technology for Re-Entry Systems in EFESTO project. In: 9th European Conference For Aeronautics And Space Science, EUCASS 2022. 9th European Conference for Aeronautics and Space Sciences (EUCASS), 27. Juni - 01. Juli 2022, Lille, Frankreich. file

  Dietlein, Ingrid Monika and Johannsson, Magni (2015) NewFex Mission Analysis. DLR-Interner Bericht. SART TN-002/2015. Other. (Unpublished) Volltext nicht online.

  Dietlein, Ingrid Monika and Schleutker, Thorn and Guidotti, Giuseppe and Pontijas Fuentes, Irene and Trovarelli, Federico and Gardi, Roberto and Verant, Jean-Luc and Prevereaud, Ysolde and Dauvois, Yann and Governale, Giuseppe (2022) EFESTO - advancing European hypersonic inflatable heatshield technology for Earth recovery and Mars high-mass delivery missions. Aeronautics and Aerospace Open Access Journal, pp. 59-73. MedCrave Group. ISSN 2576-4500. file

  Doekhie, Sandra (2012) Continuous Detonation Wave Engine: Literature Study. DLR-Interner Bericht. SART-TN021-2012. Diploma. DLR. 74 S. (Unpublished) Volltext nicht online.

  Doekhie, Sandra (2013) A computer-based tool for preliminary design and performance assessment of Continuous Detonation Wave Engines. Master's, TU Delft. Volltext nicht online.

  Doekhie, Sandra and Dumont, Etienne and Cervone, Angelo and Noomen, Ron (2013) A computer-based tool for preliminary design and performance assessment of Continuous Detonation Wave Engines. 5th European Conference For Aeronautics and Space Sciences, 1.-5. Jul. 2013, München, Deutschland. file

  Dominguez Calabuig, Guillermo Joaquin (2019) Conceptual Cost Estimation for Recovery and Refurbishment Operations of Reusable Launch Vehicles. Project Report. SART TN-006/2019. 74 S. Volltext nicht online.

  Dominguez Calabuig, Guillermo Joaquin and Miraux, Loïs and Wilson, Andrew Ross (2022) Environmental sustainability of future proposed space activities. Acta Astronautica. Elsevier. doi: 10.1016/j.actaastro.2022.07.034. ISSN 0094-5765. Volltext nicht online.

  Dominguez Calabuig, Guillermo Joaquin and Miraux, Loïs and Wilson, Andrew Ross and Sarritzu, Alberto and Pasini, Angelo (2022) Eco-Design of future reusable launchers: insight into their life cycle and atmospheric impact. In: 9th European Conference For Aeronautics And Space Science, EUCASS 2022. 9th European Conference for Aeronautics and Space Sciences (EUCASS), 27. Juni - 01. Juli 2022, Lille, Frankreich. file

  Dominguez Calabuig, Guillermo Joaquin and Wilken, Jascha (2022) Pre-conceptual staging trade-offs of reusable launch vehicles. In: 9th European Conference For Aeronautics And Space Science, EUCASS 2022. 9th European Conference for Aeronautics and Space Sciences (EUCASS), 27. Juni - 01. Juli 2022, Lillle, Frankreich. file

  Dumont, Etienne and Johannsson, Magni (2012) Reverse Engineering of Athena II Launcher. DLR-Interner Bericht. SART TN-016/2012. Deutsches Zentrum für Luft- und Raumfahrt. 12 S. (Unpublished) Volltext nicht online.

  Dumont, Etienne (2012) Variations of Solid Rocket Motor Preliminary Design for Small TSTO launcher. Space Propulsion 2012, 7.-10. Mai 2012, Bordeaux, Frankreich. file

  Dumont, Etienne (2014) ROBEX – ALUNIR Architecture Study. DLR-Forschungsbericht. SART TN-19/2014. DLR Bremen. (Unpublished) Volltext nicht online.

  Dumont, Etienne (2015) Adapted Production and Operation Cost Estimations based on Transcost Model for European launchers. DLR-Forschungsbericht, DLR-Interner Bericht. SART TN-002/2014. DLR Institut für Raumfahrtsysteme. 33 S. (Unpublished) Volltext nicht online.

  Dumont, Etienne (2016) Suitability of Reusability for a Lunar Re-Supply System. In: Proceedings of the 67th International Astronautical Congress. 67th International Astronautical Congress (IAC), 26.-30. Sep. 2016, Guadalajara, Mexiko. ISBN 9781510835825. filefile

  Dumont, Etienne (2013) High Thrust Stage - Literature study: storable propellant. DLR-Interner Bericht, Project Report. SART TN-007/2013. Deutsches Zentrum für Luft- und Raumfahrt. 39 S. (Unpublished) Volltext nicht online.

  Dumont, Etienne (2016) Design of a Modular Transportation System for Future Lunar Robotic Missions. Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan, Vol.14 (30), Pk_73-Pk81. JSASS. doi: 10.2322/tastj.14.Pk_73. ISSN 1884-0485. Volltext nicht online.

  Dumont, Etienne (2017) Workshop 2016 on market studies. DLR-Interner Bericht. XTRAS-RP-LAU-20161110 / SART TN015/2016. DLR. 220 S. (Unpublished) Volltext nicht online.

  Dumont, Etienne and Bauer, Carola and Clark, Vanessa and Koch, Aaron and Lange, Caroline and Bühler, Christian and Garbers, Nicole and Quantius, Dominik and Braukhane, Andy and Tsakyridis, Georgios and Bauer, Waldemar and Pakakis, Alexander and Bernabeu Peña, Marc (2014) ROBEX – ALUNIR Architecture Study Report. DLR-Interner Bericht. DLR-SART-TN019/2014 - DLR-RY-CE-R014-2014-1. Other. DLR Institut für Raumfahrtsysteme. 106 S. (Unpublished) Volltext nicht online.

  Dumont, Etienne and Burkhardt, Holger and Sippel, Martin and Johannsson, Magni and Ludwig, Carina and David, Emmanuelle (2013) Exploiting technological synergies for future launch vehicles. 4th International Conference – Space Technologies: Present and Future, 17.-19. Apr. 2013, Dnepropetrovsk, Ukraine. file

  Dumont, Etienne and David, Emmanuelle (2013) Ariane 5 ECA VA212 and Ariane 5 MEa: Updated models (Status September 2013). DLR-Interner Bericht. SART TN019-2013. DLR Institut für Raumfahrtsysteme. 39 S. (Unpublished) Volltext nicht online.

  Dumont, Etienne and Dumke, Michael (2015) EAGLE: Cold Gas Thrusters Design and Tests. DLR-Interner Bericht. SART TN-003/2015. Other. DLR: Institute of Space Systems. 17 S. (Unpublished) Volltext nicht online.

  Dumont, Etienne and Ecker, Tobias and Chavagnac, Christophe and Witte, Lars and Windelberg, Jens and Klevanski, Josef and Giagkozoglou, Sofia (2018) CALLISTO - Reusable VTVL launcher first stage demonstrator. Space Spropulsion Conference 2018, 14.-18. Mai 2018, Sevilla, Spanien. file

  Dumont, Etienne and Garbers, Nicole and Kopp, Alexander and Ludwig, Carina and Trivailo, Olga and Demming, J. (2013) High Thrust Stage Preliminary Design for storable propellant system. DLR-Interner Bericht. SART TN09-2013. DLR Bremen. (Unpublished) Volltext nicht online.

  Dumont, Etienne and Goh, Weixiong and Delbourg, Matthieu and Lizy-Destrez, Stéphanie and Le Bihan, Bastien (2017) Suitability of reusability and in-situ propellant production for a Lunar transportation system. In: Proceedings of the International Astronautical Congress, IAC. 68th International Astronautical Congress, 25-29 September 2017, Adelaide, Australia. filefile

  Dumont, Etienne and Kopp, Alexander and Ludwig, Carina and Garbers, Nicole (2014) High-Thrust in-Space Liquid Propulsion Stage: Storable Propellants. Space Propulsion 2014, 19.-22. Mai 2014, Köln, Deutschland. file

  Dumont, Etienne and Kopp, Alexander and Sippel, Martin (2010) SRP 1.2: Updates and simulation results. DLR-Interner Bericht. SART TN013/2009. DLR. 46 S. (Unpublished) Volltext nicht online.

  Dumont, Etienne and Ludwig, Carina and Kopp, Alexander and Sippel, Martin (2011) Advanced TSTO launch vehicles. 4th European Conference for Aerospace Sciences (EUCASS), 3.-8. Juli 2011, Sankt Petersburg, Russland. file

  Dumont, Etienne and Mierheim, Olaf and Chrupalla, David and Klevanski, J. and Bozic, Ognjan and Kopp, Alexander and Karl, Sebastian and Johannsson, Magni and Stief, Malte and David, Emmanuelle and Ludwig, Carina and Keiderling, David and Saile, Dominik and Poppe, Georg and Koch, Patrick and Schnepper, K. and Kirschner, Michael and Degenhardt, Richard and Schmidt, Volker and Manfletti, C. (2014) Ariane 6 PPH architecture: Critical Analysis - First iteration loop. DLR-Interner Bericht. X-TRAS TN-002/2013. 228 S. Volltext nicht online.

  Dumont, Etienne and Sippel, Martin (2015) Analysis of the attempt of launcher stage return by SpaceX’ Falcon 9. SPACEX WORKSHOP 2015, 23. April 2015, Paris, Frankreich. (Unpublished) Volltext nicht online.

  Dumont, Etienne and Sippel, Martin and David, Emmanuelle and Olga, Trivailo (2012) Potential Micro Launcher VLM. DLR-Interner Bericht. SART TN022/2011. DLR. 60 S. (Unpublished) Volltext nicht online.

  Dumont, Etienne and Stappert, Sven and Ecker, Tobias and Wilken, Jascha and Karl, Sebastian and Krummen, Sven and Sippel, Martin (2017) Evaluation of Future Ariane Reusable VTOL Booster stages. In: Proceedings of the International Astronautical Congress, IAC. 68th International Astronautical Congress, 25-29 September 2017, Adelaide, Australia. filefile

  Dumont, Etienne and van Foreest, Arnold and Sippel, Martin (2010) Launcher Pre-Design: VENUS II P100 + Z40 / Z35 / Z30 + Aestus II Upper Stage. Project Report. SART TN-001/2010. DLR Institut für Raumfahrtsysteme. 83 S. (Unpublished) Volltext nicht online.

  Dumont, Etienne and van Foreest, Arnold and Sippel, Martin (2010) Launcher Pre-Design: VENUS II P80/P100 + Z23 + Z9A + AVUM II. Project Report. SART TN-004/2010. DLR Institut für Raumfahrtsysteme. 77 S. (Unpublished) Volltext nicht online.

  Dumont, Etienne and van Foreest, Arnold and Sippel, Martin (2011) Launcher Pre-Design: VENUS II - Trajectory optimisation with ASTOS. DLR-Interner Bericht, Project Report. SART TN001/2011. Other. DLR. 40 S. Volltext nicht online.

  da Silveira, Guilherme (2020) INVESTIGATION OF VL-X2 PERFORMANCE USING DLR-SART METHODOLOGY. Other. SART TN-009/2020. Other. 107 S. (Unpublished) Volltext nicht online.

  da Silveira, Guilherme (2020) COMPARISON OF TOSCA AND ASTOS OPTIMAL SOLUTIONS FOR THE ASCENT FLIGHT OF A SMALL LAUNCH VEHICLE. Project Report. SART TN-007/2020. 25 S. Volltext nicht online.

  de Prenter, Frits and Verhoosel, Clemens V. and van Brummelen, Harald and Evans, John and Messe, Christian and Benzaken, Joseph and Maute, Kurt (2019) Multigrid solvers for immersed finite element methods and immersed isogeometric analysis. Computational Mechanics. Springer. doi: 10.1007/s00466-019-01796-y. ISSN 0178-7675. file

E

  Ecker, Tobias and Karl, Sebastian and Dumont, Etienne and Stappert, Sven and Krause, Daniel (2017) A Numerical Study on the Thermal Loads During a Supersonic Rocket Retro-Propulsion Maneuver. In: 53nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016. 53rd AIAA/SAE/ASEE Joint Propulsion Conference, 10.-12. Juni 2017, Atlanta, USA. doi: 10.2514/6.2017-4878. Volltext nicht frei. file

  Ecker, Tobias and Karl, Sebastian and Dumont, Etienne and Stappert, Sven and Krause, Daniel (2019) Numerical Study on the Thermal Loads During a Supersonic Rocket Retropropulsion Maneuver. Journal of Spacecraft and Rockets, 57 (1), pp. 131-146. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.A34486. ISSN 0022-4650. Volltext nicht online.

  Ecker, Tobias and Zilker, Franziska and Dumont, Etienne and Karl, Sebastian and Hannemann, Klaus (2018) Aerothermal Analysis of Reusable Launcher Systems during Retro-Propulsion Reentry and Landing. Space Propulsion Conference 2018, 14.-18. Mai 2018, Sevilla, Spanien. file

F

  Fischer, Philipp M. and Deshmukh, Meenakshi and Koch, Aaron and Mischke, Robert and Martelo Gomez, Antonio and Schreiber, Andreas and Gerndt, Andreas (2018) Enabling a Conceptual Data Model and Workflow Integration Environment for Concurrent Launch Vehicle Analysis. In: Proceedings of the International Astronautical Congress, IAC. 69th International Astronautical Congress (IAC), 1.-5. Oct. 2018, Bremen, Germany. file

  Förster, Gero and Dumont, Etienne (2017) Tosca 1.261 & rts 1.21 Validierung. DLR-Interner Bericht. SART TN-009/2016. Other. Institut für Raumfahrtsysteme. 62 S. (Unpublished) Volltext nicht online.

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  Gamgami, Farid (2009) A Trendsetting Micro-Launcher for Europe. 3rd EUCASS 2009, 6-9 Juli 2009, Versailles Frankreich. (Unpublished) file

  Gamgami, Farid and Sinnhuber, Miriam and Palm, Mathias and von Savigny, Christian (2009) IN-SITU EXPLORATION OF EARTH’S ATMOSPHERE USING NOVEL SPACECRAFT DESIGN. 60th IAC 2009, 12-16 Oktober, Daejeon Republic of Korea. (Unpublished) file

  Gamgami, Farid and Sippel, Martin and Dumont, Etienne (2010) Statistical Analysis and Classification of rocket motor efficiency, thrust to mass ratio and structural index. DLR-Interner Bericht. DLR-IB 647-2009/07. Other. DLR. 51 S. Volltext nicht online.

  Garbers, Nicole (2013) Latest version of SpaceLiner’s TPS with TOP. DLR-Interner Bericht. SART TN26-2013. DLR Bremen. (Unpublished) Volltext nicht online.

  Garbers, Nicole (2013) Passenger Capsule Window Design for SpaceLiner 7. DLR-Interner Bericht. SART TN15-2013. DLR Bremen. (Unpublished) Volltext nicht online.

  Garbers, Nicole (2013) Overall Preliminary Design of the Thermal Protection System for a Long Range Hypersonic Rocket-Powered Passenger Vehicle (SpaceLiner). 7th European Workshop on Thermal Protection Systems and Hot Structures, 8 - 10 April 2013, ESA-ESTEC, Noordwijk, The Netherlands. (Unpublished) Volltext nicht frei. file

  Garbers, Nicole (2014) Thermal protection system Optimization Program Version 2 (TOP2). DLR-Interner Bericht. SART TN-09/2014. DLR Bremen. (Unpublished) Volltext nicht online.

  Garbers, Nicole (2014) Metallic Thermal Protection System for SpaceLiner. DLR-Forschungsbericht. SART TN-16/2014. DLR Bremen. (Unpublished) Volltext nicht online.

  Garbers, Nicole (2016) Metallic TPS Design for SpaceLiner. DLR-Interner Bericht. SART TN-011/2016. DLR. (Unpublished) Volltext nicht online.

  Garbers, Nicole (2014) Metallic Thermal Protection System for SpaceLiner. DLR-Interner Bericht. SART TN-016/2014. Other. DLR. (Unpublished) Volltext nicht online.

  Goh, Weixiong (2017) PRELIMINARY DESIGN OF REUSABLE LUNAR LANDER LANDING SYSTEM. Master's, Luleå University of Technology. Volltext nicht online.

  Gori, Oscar (2019) Investigation on SpaceLiner Booster Configuration with Variable Wings. Magisterarbeit, Politecnico Turino. Volltext nicht online.

  Grundmann, Jan Thimo and Bauer, Waldemar and Biele, J. and Boden, Ralf and Ceriotti, Matteo and Cordero, Federico and Dachwald, Bernd and Dumont, Etienne and Grimm, Christian and Hercik, David and Ho, Tra-Mi and Jahnke, Rico and Koch, Aaron and Koncz, Alexander and Krause, C. and Lange, Caroline and Lichtenheldt, Roy and Maiwald, Volker and Mikschl, Tobias and Mikulz, Eugen and Montenegro, Sergio and Pelivan, Ivanka and Peloni, Alessandro and Quantius, Dominik and Reershemius, Siebo and Renger, Thomas and Riemann, Johannes and Ruffer, Michael and Sasaki, Kaname and Schmitz, Nicole and Seboldt, W. and Seefeldt, Patric and Spietz, Peter and Spröwitz, Tom and Sznajder, Maciej and Tardivel, Simon and Toth, Norbert and Wejmo, Elisabet and Wolff, Friederike and Ziach, C. (2019) Capabilities of GOSSAMER-1 derived Small Spacecraft Solar Sails carrying MASCOT-derived Nanolanders for In-Situ Surveying of NEAs. Acta Astronautica. Elsevier. doi: 10.1016/j.actaastro.2018.03.019. ISSN 0094-5765. file

  Grundmann, Jan Thimo and Bauer, Waldemar and Biele, Jens and Boden, Ralf and Borchers, Kai and Ceriotti, Matteo and Cordero, Federico and Dachwald, Bernd and Dumont, Etienne and Grimm, Christian and Hercik, David and Ho, Tra-Mi and Jahnke, Rico and Koch, Aaron and Koncz, Alexander and Krause, Christian and Lange, Caroline and Lichtenheldt, Roy and Maiwald, Volker and Mikschl, Tobias and Mikulz, Eugen and Montenegro, Sergio and Pelivan, Ivanka and Peloni, Alessandro and Quantius, Dominik and Reershemius, Siebo and Renger, Thomas and Riemann, Johannes and Ruffer, Michael and Sasaki, Kaname and Schmitz, Nicole and Seboldt, Wolfgang and Seefeldt, Patric and Spietz, Peter and Spröwitz, Tom and Sznajder, Maciej and Tardivel, Simon and Toth, Norbert and Wejmo, Elisabet and Wolff, Friederike and Ziach, Christian (2018) Small Spacecraft Solar Sailing for Small Solar System Body Multiple Rendezvous and Landing. 2018 IEEE Arospace Conference, 3.-10. Mär. 2018, Big Sky, Montana, USA. (Unpublished) file

  Grundmann, Jan Thimo and Bauer, Waldemar and Biele, Jens and Boden, Ralf and Borchers, Kai and Ceriotti, Matteo and Cordero, Federico and Dachwald, Bernd and Dumont, Etienne and Grimm, Christian and Hercik, David and Ho, Tra-Mi and Jahnke, Rico and Koch, Aaron D. and Koncz, Alexander and Krause, Christian and Lange, Caroline and Lichtenheldt, Roy and Maiwald, Volker and McInnes, Colin and Meß, Jan-Gerd and Mikschl, Tobias and Mikulz, Eugen and Montenegro, Sergio and Pelivan, Ivanka and Peloni, Alessandro and Quantius, Dominik and Reershemius, Siebo and Renger, Thomas and Riemann, Johannes and Ruffer, Michael and Sasaki, Kaname and Schmitz, Nicole and Seboldt, Wolfgang and Seefeldt, Patric and Spietz, Peter and Spröwitz, Tom and Sznajder, Maciej and Tardivel, Simon and Toth, Norbert and Wejmo, Elisabet and Wolff, Friederike and Ziach, C. (2019) Solar Sails for Planetary Defense & High-Energy Missions. In: 2019 IEEE Aerospace Conference, AERO 2019. 40th IEEE Aerospace Conference 2019, 02.-09. Mär. 2019, Big Sky, Montana, U.S.A.. doi: 10.1109/AERO.2019.8741900. ISSN 1095-323X. filefile

  Grundmann, Jan Thimo and Bauer, Waldemar and Biele, Jens and Boden, Ralf and Ceriotti, Matteo and Cordero, Federico and Dachwald, Bernd and Dumont, Etienne and Grimm, Christian and Hercik, David and Herique, Alain and Ho, Tra-Mi and Jahnke, Rico and Koch, Aaron and Kofman, Wlodek and Koncz, Alexander and Krause, Christian and Lange, Caroline and Lichtenheldt, Roy and Maiwald, Volker and Mikschl, Tobias and Mikulz, Eugen and Montenegro, Sergio and Pelivan, Ivanka and Peloni, Alessandro and Plettemeier, Dirk and Quantius, Dominik and Reershemius, Siebo and Renger, Thomas and Riemann, Johannes and Ruffer, Michael and Sasaki, Kaname and Schmitz, Nicole and Seboldt, Wolfgang and Seefeldt, Patric and Spietz, Peter and Spröwitz, Tom and Sznajder, Maciej and Tardivel, Simon and Toth, Norbert and Wejmo, Elisabet and Wolff, Friederike and Ziach, Christian (2018) Efficient Massively Parallel Prospection for ISRU by Multiple Near-Earth Asteroid Rendezvous using Near-Term Solar Sails and 'Now-Term' Small Spacecraft Solutions. In: Asteroid Science Intersections with In-Space Mine Engineering – Abstracts. 2nd Asteroid Science Intersections with In-Space Mine Engineering – ASIME 2018, 16.-17. Apr. 2018, Belval, Luxembourg. filefile

  Grundmann, Jan Thimo and Biele, Jens and Dachwald, Bernd and Grimm, Christian and Lange, Caroline and Ulamec, Stephan and Ziach, Christian and Spröwitz, Tom and Ruffer, Michael and Seefeldt, Patric and Spietz, Peter and Toth, Norbert and Kawaguchi, J. and Mori, O. and Rittweger, Andreas and Bibring, Jean-Pierre and Braukhane, Andy and Boden, Ralf and Chujo, Toshihiro and Dumont, Etienne and Jahnke, Stephan Siegfried and Jetzschmann, Michael and Kato, H and Krüger, Hans and Lange, Michael and Martelo Gomez, Antonio and Massonett, Didier and Mimasu, Yuya and Okada, T. and Sagliano, Marco and Sasaki, Kaname and Schröder, Silvio and Sippel, Martin and Skoczylas, Thomas and Wejmo, Elisabet (2017) Small Landers and Separable Sub-Spacecraft for Near-term Solar Sails. The Fourth International Symposium on Solar Sailing 2017, 17.-20. Jan. 2017, Kyoto, Japan. filefilefile

  Grundmann, Jan Thimo and Boden, Ralf and Ceriotti, Matteo and Dachwald, Bernd and Dumont, Etienne and Grimm, Christian and Lange, Caroline and Lichtenheldt, Roy and Pelivan, Ivanka and Peloni, Alessandro and Riemann, Johannes and Spröwitz, Tom and Tardivel, Simon (2017) Soil to Sail - Asteroid Landers on Near-Term Sailcraft as an Evolution of the Gossamer Small Spacecraft Solar Sail Concept for In-Situ Characterization. 5th IAA Planetary Defense Conference 2017, 15.-19. Mai 2017, Tokyo, Japan. filefilefilefilefile

  Grundmann, Jan Thimo and Lange, Caroline and Dachwald, Bernd and Grimm, Christian and Koch, Aaron and Ulamec, Stephan (2015) Small Spacecraft in Planetary Defence Related Applications – Capabilities, Constraints, Challenges. In: nicht gedruckt. IEEE. 2015 IEEE Aerospace Conference, 7.-13. Mar. 2015, Big Sky, Montana, USA. file

  Guidotti, Guiseppe and Pontijas Fuentes, Irene and Trovarelli, Federico and Dietlein, Ingrid Monika and Callsen, Steffen and Bergmann, Kevin and Verant, Jean-Luc and Gardi, Roberto and Gambacciani, Giovanni and Governale, Guiseppe (2022) The EFESTO Project: Advanced European Re-Entry System based on Inflatable Heat Shield. In: 2nd International Conference on Flight Vehicles, Aerothermodynamics and Re-Entry Missions & Engineering (FAR). 2nd International Conference on Flight Vehicles, Aerothermodynamics and Re-Entry Missions & Engineering (FAR), 19.-23. Juni 2022, Heilbronn, Deutschland. file

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  Haferkamp, Jan-René (2019) Vorauslegung und numerische Berechnung der Vorbrennkammern der SpaceLiner Main Engines (SLME) und Integration in die Turbopumpenanordnung (Integrated Power Head). Bachelor's, Hochschule Bremen. Volltext nicht online.

  Haya-Ramos, Rodrigo and de Zaiacomo, Gabriele and Freixa, Jordi and Sippel, Martin and Molina, Rafael (2012) GNC requirements of for a Long Range Hypersonic Transport System. American Institute of Aeronautics and Astronautics. 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference, 24.-28. Sep. 2012, Tours, France. ISBN 978-1-60086-931-0. file

  Hebborn, Nils (2022) A Systematic Analysis of First Stage Recovery Options for Two Small-Sat Launch Vehicles (Microlaunchers). Master's, Technische Universität München. Volltext nicht online.

  Hurlbert, Eric A. and Manfletti, Chiara and Sippel, Martin (2016) International Space Exploration Coordination Group Assessment of Technology Gaps for LOx/Methane Propulsion Systems for the Global Exploration Roadmap. AIAA SPACE 2016, 13. - 16. September 2016, Long Beach, California. doi: 10.2514/6.2016-5280. ISBN 978-162410427-5. file

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  Jain, Minal (2022) Study of Structural Design Concepts for small-scale Aircraft using low-cost Manufacturing Techniques. Master's, Universität Bremen. Volltext nicht online.

  Johannsson, Magni (2012) Optimization of Solid Rocket Grain Geometries. Master's, Kungliga Tekniska Högskolan/DLR-SART. Volltext nicht online.

  Johannsson, Magni (2012) Capsule Rescue Motors for SpaceLiner 7.1. DLR-Interner Bericht. SART TN-018/2012. Deutsches Zentrum für Luft- und Raumfahrt. 18 S. (Unpublished) Volltext nicht online.

  Johannsson, Magni (2013) Visualization of Solid Rocket Motors with VRML 2.0. DLR-Interner Bericht. SART TN12-2013. DLR Bremen. (Unpublished) Volltext nicht online.

  Johannsson, Magni (2013) Critical Analysis of ESA’s Ariane 6 Linear Multi-Booster Configuration. DLR-Interner Bericht. SART TN21-2013. DLR Bremen. (Unpublished) Volltext nicht online.

  Johannsson, Magni and Clark, Vanessa Jane (2015) Critical Analyses and Performance Validation of the SKYLON D1 Space Plane. DLR-Interner Bericht. SART TN-027/2014. Other. DLR. (Unpublished) Volltext nicht online.

  Johannsson, Magni and Dumont, Etienne and Clark, Vanessa and David, Emmanuelle and Sippel, Martin (2016) Launcher Pre-Design: ANGELA: A Next GEneration LAuncher - Trajectory and Payload Optimisation. Project Report. SART TN006/2013. DLR: Institut für Raumfahrtsysteme. 104 S. (Unpublished) Volltext nicht online.

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  Kaltenhäuser, Sven and Klünker, Carmo Sonja and Schmitt, Dirk-Roger and Sippel, Martin and Veth, Jürgen and Zimmermann, Kai and Lockheed Jr., Allan H. and Strom, John R. (2020) Machbarkeitsstudie Spaceport Rostock-Laage. Studie im Auftrag des Ministeriums für Energie, Infrastruktur und Digitalisierung Mecklenburg-Vorpommern und des Ministeriums für Bildung, Wissenschaft und Kultur Mecklenburg-Vorpommern. [Other] filefile

  Kaltenhäuser, Sven and Klünker, Carmo Sonja and Schmitt, Dirk-Roger and Sippel, Martin and Veth, Jürgen and Zimmermann, Kai and Lockheed Jr., Allan H. and Strom, John R. (2020) Spaceport Concept in Germany. In: Proceedings of the International Astronautical Congress, IAC. International Astronautical Federation. 71th International Aeronatical Congress - IAC, 12. -14. October 2020, The CyberSpace Edition. ISSN 0074-1795. file

  Kaltenhäuser, Sven and Klünker, Carmo Sonja and Schmitt, Dirk-Roger and Sippel, Martin and Veth, Jürgen and Zimmermann, Kai and Lockheed Jr., Allan H. and Strom, John R. (2020) Machbarkeitsstudie Spaceport Rostock-Laage. 86. Stizung des Energieausschusses des Landtages Mecklenburg-Vorpommern, 16. September 2020, Schwerin. Volltext nicht online.

  Kaltenhäuser, Sven and Klünker, Carmo Sonja and Schmitt, Dirk-Roger and Sippel, Martin and Veth, Jürgen and Zimmermann, Kai and Lockheed Jr., Allan H. and Strom, John R. (2020) Spaceport Rostock-Laage - Die nächsten Schritte. Entwicklungsworkshop Flughafen Rostock-Laage, 26. Oktober 2020, Rostock. Volltext nicht online.

  Karl, Sebastian and Wilken, Jascha and Bussler, Leonid (2022) Aerothermal Databases and Heat-Load Prediction for Re-Usable Launch Vehicle Configurations. In: HiSST, 2nd International Conference on High-Speed Vehicle Science and Technology, pp. 1-14. CEAS. 2nd International Conference on High-Speed Vehicle Science & Technology, 11.-15. Sept. 2022, Brügge, Belgien. Volltext nicht frei. file

  Klevanski, Josef and Ecker, Tobias and Riehmer, Johannes and Reimann, Bodo and Dumont, Etienne and Chavagnac, Christophe (2018) Aerodynamic Studies in Preparation for CALLISTO - Reusable VTVL Launcher First Stage Demonstrator. 69th International Astronautical Congress (IAC), 1-5 October 2018, Bremen, Germany. file

  Koch, A. (2009) Stochastic variation of a sharp-edged re-entry vehicle. 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, 19-22 Oct 2009, Bremen, Germany. file

  Koch, Aaron and Bauer, C. and Dumont, Etienne and Minutolo, F. and Sippel, M. and Grenard, P. and Ordonneau, G. and Winkler, H. and Guénot, L. and Linck, C. and Wood, C.R. and Vira, J. and Sofiev, M. and Tarvainen, V. (2013) Multidisciplinary approach for assessing the atmospheric impact of launchers. In: CEAS 2013 Air & Space Conference, pp. 340-346. Linköping University Electronic Press. CEAS 2013 Air & Space Conference, 15.-19. Dez. 2013, Linköping, Finnland. ISBN 9789175195193. file

  Koch, Aaron and Bauer, Carola and David, Emmanuelle and Dumont, Etienne and Garbers, Nicole and Herbertz, A. and Johannsson, Magni and Ludwig, Carina and Manfletti, C. (2015) META CE Workshop: Technical Note. DLR-Interner Bericht. XTRAS-TN-METACE-20140303 & SART TN-011/2014. Other. DLR. 126 S. (Unpublished) Volltext nicht online.

  Koch, Aaron D. (2019) Optimal staging of serially staged rockets with velocity losses and fairing separation. Aerospace Science and Technology, 88, pp. 65-72. Elsevier. doi: 10.1016/j.ast.2019.03.019. ISSN 1270-9638. Volltext nicht online.

  Koch, Aaron D. (2019) Fast, robust and near-optimal approximation of GTO trajectories and payload capacities of multistage rockets. CEAS Space Journal, 11 (3), pp. 269-285. Springer. doi: 10.1007/s12567-019-00244-0. ISSN 1868-2502. Volltext nicht online.

  Koch, Aaron Dexter (2021) Staging and trajectory optimization of rockets during conceptual design. Dissertation, Universität Bremen. Volltext nicht online.

  Kopp, Alexander (2012) PARAMETRIC STUDIES FOR THE STRUCTURAL PRE-DESIGN OF HYPERSONIC AEROSPACE VEHICLES. In: Proceedings of 12th European Conference on Spacecraft Structures, Materials and Environmental Testing. ESA. 12th European Conference on Spacecraft Structures, Materials and Environmental Testing, 20.-23. März 2012, Noordwijk, The Netherlands. file

  Kopp, Alexander and Dietlein, Ingrid and Sippel, Martin Dr. (2009) REX Free Flyer Systemvorentwurf Zwischenbericht. Project Report. DLR Institut für Raumfahrtsysteme. 129 S. (Unpublished) Volltext nicht online.

  Kopp, Alexander (2016) THE AURORA SPACE LAUNCHER CONCEPT. Deutsche Luft- und Raumfahrtkongress (DLRK) 2016, 13.-15. September 2016, Braunschweig, Deutschland. file

  Kopp, Alexander (2016) Hypersonic Launcher Concept Aurora – Basic Concept Formulation and Configuration R1 Preliminary System Design. DLR-Interner Bericht. SART TN-004/2016. Other. DLR. (Unpublished) Volltext nicht online.

  Kopp, Alexander (2015) Implementation of Honeycomb Sandwich Design Concepts in LSAP. DLR-Interner Bericht. SART TN-015/2015. Other. DLR. (Unpublished) Volltext nicht online.

  Kopp, Alexander (2017) DAS AURORA-R2 RLV-KONZEPT. 66. Deutsche Luft- und Raumfahrtkongress, 5.-7. September 2017, München, Deutschland. file

  Kopp, Alexander (2018) Parametric Aero-Thermo-Mechanical Investigation of a Hypersonic Transport Glider. Dissertation, Universität Braunschweig. Volltext nicht online.

  Kopp, Alexander (2018) RLV-Konfiguration Aurora-R2. DLR-Interner Bericht. DLR SART TN-004/2017. Other. DLR. 183 S. (Unpublished) Volltext nicht online.

  Kopp, Alexander and Bussler, Leonid (2018) Validierung der Aerodynamik und Aerothermodynamik Analyseprozeduren des Hotsose Codes Version 1.91. Project Report. SART TN-006/2017. 35 S. Volltext nicht online.

  Kopp, Alexander and Dietlein, Ingrid and Barth, Tarik (2009) Systemanalyse für scharfkantige Wiedereintrittsfahrzeuge. Deutscher Luft- und Raumfahrtkongress 2009, 08.-10. Sep. 2009, Aachen, Deutschland. file

  Kopp, Alexander and Garbers, Nicole (2014) STRUCTURAL AND TPS TRADE-OFF STUDIES AND DESIGN OPTIONS FOR THE HYPERSONIC TRANSPORT SYSTEM SPACELINER. European Conference on Spacecraft Structures, Materials & Environmental Testing, 01.-04.04.2014, Braunschweig, Deutschland. file

  Kopp, Alexander and Garbers, Nicole (2014) Investigation of Structure, Thermal Protection System, and Passenger Stage Integration for the Hypersonic Transport System SpaceLiner. 14th AIAA Aviation Technology, Integration, and Operations Conference, 16.-20.06.2014, Atlanta. file

  Kopp, Alexander and Garbers, Nicole and Jarlas, Rolf and Rabia, Hamid (2012) Parametric Structural Analysis for the SpaceLiner. In: Proceedings of 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference (AIAA 2). AIAA. 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference, 24. - 28. September 2012, Tours, France. ISSN Chapter DOI: 10.2514/6.2012-5944. file

  Kopp, Alexander and Sippel, Martin (2016) NOVEL HYPERSONIC LAUNCHER CONCEPT USING THIN-PLY CFRP COMPOSITES. 14th European Conference on Spacecraft Structures, Materials and Environmental Testing, 27.-30. Sept. 2016, Toulouse, France. file

  Kopp, Alexander and Sippel, Martin and Stappert, Sven and Darkow, Nicolas and Gerstmann, Jan and Krause, Stefan and Stefaniak, Daniel and Beerhorst, Matthias and Thiele, Thomas and Gülhan, Ali and Kronen, Rolf and Schnepper, Klaus and Briese, Lale Evrim and Riccius, Jörg (2017) FORSCHUNG AN SYSTEMEN UND TECHNOLOGIEN FÜR WIEDERVERWENDBARE RAUMTRANSPORTSYSTEME IM DLR-PROJEKT AKIRA. Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V., Bonn, 2017. Deutschen Luft- und Raumfahrtkongress (DLRK) 2017, 5.-7. September 2017, München, Deutschland. file

  Kopp, Alexander and Stappert, Sven and Mattsson, David and Olofsson, Kurt and Marklund, Erik and Kurth, Guido and Mooij, Erwin and Roorda, Evelyne (2017) The Aurora space launcher concept. CEAS Space Journal. Springer. doi: 10.1007/s12567-017-0184-2. ISSN 1868-2502. file

  Kopp, Alexander and Van Foreest, Arnold and Sippel, Martin and Dalenbring, Mats and Jarlas, Rolf (2011) Investigation of Structure for the Hypersonic Transport System SpaceLiner. In: Proceedings of the 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA. 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 11.-14. April 2011, San Francisco, USA. ISSN Chapter DOI: 10.2514/6.2011-2373. file

  Koröde, Lars (2021) Parametrische Kostenmodellierung und - Schätzung von wiederverwendbaren Trägersystemen. Bachelor's, Universität Bremen. Volltext nicht online.

  Krause, Lukas (2021) Development of cryogenic upper-stage concepts for future European launchers after Ariane 6. Magisterarbeit, Hochschule Bremen. Volltext nicht online.

  Krolikowski, Alanna and David, Emmanuelle (2012) Commercial On-Orbit Satellite Servicing and Active Debris Removal: Policy Considerations Raised by Industry Plans. IAC 2012, 1.-5. Oktober 2012, Neaple, Italien. Volltext nicht online.

  Krummen, Sven (2016) Investigation of flight dynamics and effects of rotational degrees of freedom on the flight performance of asymmetric space transportation systems based on the SpaceLiner 7 concept. DLR-Interner Bericht. SART TN-010/2016. Master's. DLR. (Unpublished) Volltext nicht online.

  Krummen, Sven and Sippel, Martin (2017) INVESTIGATION OF THE ASCENT FLIGHT DYNAMICS OF THE SPACELINER CONCEPT AS A NON-SYMMETRIC LAUNCHER CONFIGURATION. Deutscher Luft- und Raumfahrtkongress 2017, 5.-.7. September 2017, München, Deutschland. file

  Krummen, Sven and Sippel, Martin (2018) Effects Of The Rotational Vehicle Dynamics On The Ascent Flight Trajectory Of The Spaceliner Concept. CEAS Space Journal. Springer. doi: 10.1007/s12567-018-0223-7. ISSN 1868-2502. file

  Krummen, Sven and Sippel, Martin (2017) Off-Nominal Trajectories of SpaceLiner 7-3. Project Report. SART TN-014/2017. 68 S. Volltext nicht online.

  Krummen, Sven and Tummala, Pavan and Wilken, Jascha and Dumont, Etienne and Ertl, Moritz and Ecker, Tobias and Riehmer, Johannes and Klevanski, Josef (2023) Applying Bayesian Inference to Estimate Uncertainties in the Aerodynamic Database of CALLISTO. In: 2022 IEEE Aerospace Conference, AERO 2022. IEEE Aerospace Conference, 04.-11. März 2023, Big Sky, Montana, USA. ISBN 978-166543760-8. ISSN 1095-323X. (Submitted) file

L

  Lang, A. and Sippel, M. and Klevanski, J. and Atanassov, U. (2010) Atllas: M6 propulsion data set, CAD model, mass estimation and trajectory analysis. Project Report. Institute of Space Systems. (Unpublished) Volltext nicht online.

  Lang, A. and Atanassov, U. and Sippel, M. and Koch, A. (2010) ATLLAS: M3 CAD- and mass-model. Project Report. Institute of Space Systems. (Unpublished) file

  Lanzendorfer, Finn (2014) Improvement of the code “HOTSOSE” to version 1.9. DLR-Interner Bericht. SART TN-024/2014. DLR Bremen. (Unpublished) Volltext nicht online.

  Lipp, Sarah and Bauer, Carola and Trivailo, Olga (2014) Spaceport Concepts and Locations for the SpaceLiner. DLR-Interner Bericht. SART TN-022/2014. DLR Bremen. (Unpublished) Volltext nicht online.

  Lipp, Sarah and Dumont, Etienne (2017) LES Cost – A Development, Production and Operation Costs Estimation Tool based on TransCost. DLR-Interner Bericht. SART TN-008/2016. DLR. (Unpublished) Volltext nicht online.

  Lipp, Sarah and Stappert, Sven and Sippel, Martin and Dietlein, Ingrid Monika (2017) ReFEx Missionsanalyse. DLR-Interner Bericht. DLR SART TN-014/2016. Other. DLR. 113 S. (Unpublished) Volltext nicht online.

  Lipp, Sarah and Trivailo, Olga (2015) Innovation appraisal of the SpaceLiner concept. DLR-Interner Bericht. SART TN-005/2015. Bachelor's. Deutsches Zentrum für Luft- und Raumfahrt. 51 S. (Unpublished) Volltext nicht online.

  Louaas, Eric and Talbot, Chrsistoph and Gonzalez Gotor, Pilar and Ruiz Merino, Alejandro and Longo, Jose and Sippel, Martin and Froebel, Ludgar (2009) ALDEBARAN: A "SYSTEM" DEMONSTRATOR PROJECT FOR NEW GENERATIONS OF SPACE TRANSPORTATION, NOW ENTERING IN THE PHASE A. IAC (International Astronautical Federation ) 2009, 12.-16. Okt. 2009, Daejeon, Korea. file

  Ludwig, Carina and Dreyer, Michael (2013) Analyses of Cryogenic Propellant Tank Pressurization based upon Experiments and Numerical Simulations. In: 5TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS). 5th EUCASS, 01.-05.07.2013, München. file

  Ludwig, Carina and Dreyer, Michael and Hopfinger, E.J (2013) Pressure variations in a cryogenic liquid storage tank subjected to periodic excitations. International Journal of Heat and Mass Transfer, pp. 223-234. Elsevier. doi: 10.1016/j.ijheatmasstransfer.2013.06.072. ISSN 0017-9310. Volltext nicht online.

  Ludwig, Carina (2014) Analysis of Cryogenic Propellant Tank Pressurization based upon Experiments and Numerical Simulations. Dissertation, University of Bremen. Volltext nicht online.

  Ludwig, Carina and Dreyer, Michael (2012) Analyses of Cryogenic Propellant Tank Pressurization based upon Ground Experiments. American Institute of Aeronautics and Astronautics. AIAA SPACE 2012 Conference & Exposition, 11.-13. Sep. 2012, Pasadena, California, USA. ISBN 978-1-60086-940-2. file

  Ludwig, Carina and Dreyer, Michael (2014) Investigations on thermodynamic phenomena of the active-pressurization process of a cryogenic propellant tank. Cryogenics, 63, pp. 1-16. Elsevier. doi: 10.1016/j.cryogenics.2014.05.005. ISSN 0011-2275. Volltext nicht online.

M

  Maj, Ingolf (2022) Sensitivitätsanalyse von zweistufigen Trägerraketen in Hinblick auf Auswirkungen auf Massenbudgets. Master's, Universität Bremen. Volltext nicht online.

  Manfletti, Chiara and Koch, Aaron (2015) META CEF Study. DLR-Interner Bericht. SART TN-011/2014. Other. DLR. (Unpublished) Volltext nicht online.

  Messe, Christian (2020) Theoretical Fundamentals and Suggestions of Improvement for the HOTSOSE program. Project Report. SART TN-013/2019. 50 S. Volltext nicht online.

  Meyer, Frank (2014) Vorentwurfsuntersuchungen zur aktiven Kühlung thermisch hochbelasteter Regionen am Hyperschall-Passagiertransportkonzept SpaceLiner Dieser Bericht enthält: 87 Seiten einschl. 66 Abbildungen 17 Tabellen 43 Literaturzitate 05.06.2014 10:40:00 Deutsches Zentrum für Luft- und Raumfahrt e.V. Institut für Raumfahrtsysteme Systemanalyse Raumtransport (SART) 28359. DLR-Interner Bericht. SART TN-07/2014. DLR Bremen. (Unpublished) Volltext nicht online.

  Mokstadt, Johann (2014) Untersuchung der Rettungskapsel-Separationsmechanismen für das Hyperschallverkehrsflugzeug SpaceLiner. DLR-Interner Bericht. Bachelor's. DLR Institut für Raumfahrtsysteme, Bremen. Volltext nicht online.

  Mokstadt, Johann (2013) Modellierung des Boosters SL7-3 in CATIA V5 R20. DLR-Interner Bericht. SART TN-003/2013. DLR Bremen. (Unpublished) Volltext nicht online.

  Montani, Augusto (2014) A Grain Burnback Analysis Model for Solid Rocket Motor Preliminary Design. DLR-Interner Bericht. SART TN-18/2014. Bachelor's. DLR Bremen. (Unpublished) Volltext nicht online.

N

  Naranjo Amaya, Javier Eduardo (2021) Comparison of Lagrange-based CFD methods with Euler-based methods for two-dimensional simulation of sloshing in tanks and evaluation of three-dimensional effects for selected test cases. Master's, Universität Bremen. Volltext nicht online.

  Noel, L. and Schmidt, M. and Messe, Christian and Evans, J.A. and Maute, Kurt (2020) Adaptive level set topology optimization using hierarchical B-splines. Structural and Multidisciplinary Optimization. Springer. doi: 10.1007/s00158-020-02584-6. ISSN 1615-147X. Volltext nicht online.

O

  Okai, Keiichi and Sippel, Martin (2007) Component Analysis of TBCC Propulsion for a Mach 4.5 Supersonic Cruise Airliner. EUCASS, 01.-06. Jul 2007, Brussels, Belgium. file

P

  Palli, Marco (2018) Study of different options for Cabin Rescue System of SpaceLiner. Master's, Politecnico Turino. Volltext nicht online.

  Peris Marti, Izan (2015) Structural analysis and design of a truss connecting structure for the Space Liner booster. DLR-Interner Bericht. SART TN-008/2015. Other. (Unpublished) Volltext nicht online.

  Peris Martí, Izan (2015) System Studies for reusable SSTO Space Transportation Systems. DLR-Interner Bericht. SART TN-001/2015. Master's. DLR. (Unpublished) Volltext nicht online.

  Petrović, Stacha and Dumont, Etienne (2015) Lunar Landing Simulations With Tosca. DLR-Forschungsbericht, DLR-Interner Bericht. SART TN-006/2015. Other. DLR Institut für Raumfahrtsysteme. 165 S. (Unpublished) Volltext nicht online.

  Pouplin, Jennifer and Dumont, Etienne (2016) Falcon 9 v1.1 and v1.2 performances and first stage descent/return trajectories analyses. DLR-Interner Bericht. DLR-IB-RY-HB-2016-51. Other. DLR Institut für Raumfahrtsysteme. 74 S. (Unpublished) Volltext nicht online.

R

  Rauh, Carolin and Reimer, Thomas and Sippel, Martin (2019) Investigation of an RLV Cryogenic Tank Insulation Including a Purge Gap System. FAR 2019, 30. Sept. - 03. Okt. 2019, Monopoli, Italien. (Unpublished) Volltext nicht online.

  Rauh, Carolin and Reimer, Thomas and Wilken, Jascha (2022) Leakage Investigation of Epoxy-Based Composite Laminates for Reusable Cryogenic Propellant Tanks. 2nd International Conference on Flight Vehicles, Aerothermodynamics and Re-entry Missions & Engineering (FAR), 19.-23. Juni 2022, Heilbronn, Deutschland. file

  Reimer, Thomas and Kuhn, Markus and Gülhan, Ali and Esser, Burkard and Sippel, Martin and van Foreest, Arnold (2011) Transpiration Cooling Tests of Porous CMC in Hypersonic Flow. 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 11.-14. Apr 2011, San Francisco, USA. file

  Reimer, Thomas and Rauh, Carolin and Di Martino, Giuseppe and Sippel, Martin (2022) Thermal investigation of a purged insulation system for a reusable cryogenic tank. Journal of Spacecraft and Rockets, 59 (4), pp. 1205-1213. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.A35252. ISSN 0022-4650. Volltext nicht frei. file

  Rickmers, Peter and Bauer, Waldemar and Sippel, M. and Stappert, Sven and Schwarz, René and Sagliano, Marco and Trigo, Guilherme Fragoso and Wübbels, Guido and Martens, Hauke (2018) An Update of the Upcoming DLR Reusability Flight Experiment - ReFEx. In: Proceedings of the International Astronautical Congress, IAC. 69th International Astronautical Congress (IAC), 1.-5. Okt. 2018, Bremen. Volltext nicht frei. file

  Rickmers, Peter and Bauer, Waldemar and Sippel, Martin and Stappert, Sven (2017) ReFEx: Reusability Flight Experiment A Flight Experiment to Demonstrate Controlled Aerodynamic Flight from Hypersonic to Subsonic Velocities with a Winged RLV. In: 7TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS). 7TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS), 3.-6. July 2017, Milan, Italien. Volltext nicht frei. file

  Rickmers, Peter and Bauer, Waldemar and Stappert, Sven and Kiehn, Daniel and Sippel, Martin (2018) Current status of the DLR Reusability Flight Experiment - ReFEx. HiSST: International Conference on High-Speed Vehicle Science Technology, 26.-29. November 2018, Moskau. Volltext nicht frei. file

  Rickmers, Peter and Bauer, Waldemar and Wenzel, Andreas and Stappert, Sven and Wartemann, Viola and Wübbels, Guido and Acquatella B., Paul and Schmidt, Alexander (2020) Reusability Flight Experiment (ReFEx): Flight Safety Analyses. Project Report. RFX-ENG-006, SART TN-005/2020. 95 S. Volltext nicht online.

  Rickmers, Peter and Schmidt, Alexander and Kirchhartz, Rainer and Bauer, Waldemar and Stappert, Sven (2019) THE DLR REUSABILITY FLIGHT EXPERIMENT (REFEX) – CHALLENGES OF FLYING AN AERODYNAMICALLY GUIDED EXPERIMENT ON AN UNGUIDED SOUNDING ROCKET. 24TH ESA SYMPOSIUM ON EUROPEAN ROCKET AND BALLOON PROGRAMMES AND RELATED RESEARCH, 16.-20. Juni 2019, Essen, Deutschland. Volltext nicht frei. file

  Roorda, Evelyne (2016) Configuration and Preliminary Design Studies for the “LEO Fracht Transporter” (LFT) Concept. Other. SART TN-016/2015. Other. DLR. (Unpublished) Volltext nicht online.

  Roorda, Evelyne (2018) Thermal Protection System Analysis and Sizing for Spaceplane Configurations. DLR-Interner Bericht. DLR SART TN-016/2017. Other. DLR. 144 S. (Unpublished) Volltext nicht online.

S

  Schulz, Fabian (2019) Dynamic Graph Supported Object Mapping in Python. Bachelor's, Hochschule Emden/Leer. Volltext nicht online.

  Schwanekamp, Tobias and Bauer, Carola and Kopp, Alexander (2012) The Development of the SpaceLiner Concept and its Latest Progress. In: 4TH CSA-IAA CONFERENCE ON ADVANCED SPACE TECHNOLOGY. 4TH CSA-IAA CONFERENCE ON ADVANCED SPACE TECHNOLOGY, 05.-08. Sep. 2012, Shanghai, China. file

  Schwanekamp, Tobias and Bütünley, Jochen and Sippel, Martin (2012) Preliminary Multidisciplinary Design Studies on an Upgraded 100 Passenger SpaceLiner Derivative. 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference, 24.-28. Sep. 2012, Tours, Frankreich. file

  Schwanekamp, Tobias and Garbers, Nicole and Sippel, Martin (2015) CONCEPTUAL DESIGN OF THE SPACELINER THERMAL PROTECTION SYSTEM. 8th European Symposium on Aerothermodynamics for Space Vehicles, 2.3-6.3.2015, Lissabon, Portugal. file

  Schwanekamp, Tobias and Ludwig, Carina and Sippel, Martin (2014) Cryogenic Propellant Tank and Feedline Design Studies in the Framework of the CHATT Project. In: 19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. Deutsches Zentrum für Luft- und Raumfahrt (DLR). 19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 16.-20. Juni 2014, Atlanta, GA, USA. file

  Schwanekamp, Tobias and Meyer, Frank and Reimer, Thomas and Petkov, Ivaylo and Tröltzsch, Anke and Siggel, Martin (2014) System Studies on Active Thermal Protection of a Hypersonic Suborbital Passenger Transport Vehicle. In: 19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA. 19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 16.-20. Juni 2014, Atlanta, GA, USA.

  Schwanekamp, Tobias and Sippel, Martin (2015) The SpaceLiner Hypersonic System – Aerothermodynamic Requirements and Design Process. 8th European Symposium on Aerothermodynamics for Space Vehicles, 2.3-6.3.2015, Lissabon, Portugal. file

  Singh, Sunayna and Bussler, Leonid and Callsen, Steffen and Stappert, Sven and Lopes, Silvania and Buckingham, Sophia (2022) A Superposition Approach to Aerodynamic Modelling of a Capturing Device used for In-Air Capturing of a Reusable Launch Vehicle. In: 9th European Conference For Aeronautics And Space Science, EUCASS 2022. 9th European Conference for Aeronautics and Space Sciences (EUCASS), 27. Juni - 01. Juli 2022, Lille, Frankreich. file

  Singh, Sunayna and Bussler, Leonid and Stappert, Sven and Sippel, Martin and Kucukosman, Yakut Cansev and Buckingham, Sophia (2022) Simulation and Analysis of Pull-Up Manoeuvre during In-Air Capturing of a Reusable Launch Vehicle. In: 9th European Conference For Aeronautics And Space Science, EUCASS 2022. 9th European Conference for Aeronautics and Space Sciences (EUCASS), 27. Juni - 01. Juli 2022, Lille, Frankreich. file

  Singh, Sunayna and Mooij, Erwin (2020) Robust Control For Active Debris Removal of a Large Flexible Space Structure. In: AIAA Scitech 2020 Forum. AIAA Guidance, Navigation and Control Conference, 6-10 January, Orlando, Florida. doi: 10.2514/6.2020-2077. ISBN 978-162410595-1. ISSN 2020-2077. Volltext nicht frei. file

  Singh, Sunayna and Simioana, Madalin (2022) FULL SCALE SIMULATION OF IN-AIR CAPTURING. VKI Lecture Series, 25.-27.04.2022, Sint-Genesius-Rode, Belgien. Volltext nicht online.

  Singh, Sunayna and Simioana, Madalin and Stappert, Sven and Sippel, Martin and Buckingham, Sophia and Lopes, Silvania and Kucukosman, Yakut Cansev (2022) Control Design and Analysis of a Capturing Device Performing In-Air Capturing of a Reusable Launch Vehicle. In: 9th European Conference For Aeronautics And Space Science, EUCASS 2022. 9th European Conference for Aeronautics and Space Sciences (EUCASS), 27. Juni - 01. Juli 2022, Lille, Frankreich. file

  Singh, Sunayna and Stappert, Sven (2020) Falcon 9 Block 5 and Falcon Heavy Block 5 Launcher and Mission Analysis. Project Report. SART TN-018/2019. 76 S. Volltext nicht online.

  Singh, Sunayna and Stappert, Sven and Buckingham, Sophia and Lopes, Silvania and Kucukosman, Yakut Cansev and Simioana, Madalin and Pripasu, Mihai and Wiegand, Andreas and Sippel, Martin and Planquart, Philippe (2021) DYNAMIC MODELLING AND CONTROL OF AN AERODYNAMICALLY CONTROLLED CAPTURING DEVICE FOR ‘IN-AIR-CAPTURING’ OF A REUSABLE LAUNCH VEHICLE. In: 11th International ESA Conference on Guidance, Navigation & Control Systems. 11th International ESA Conference on Guidance, Navigation & Control Systems, 22-25 June 2021, Online. file

  Singh, Sunayna and Stappert, Sven and Bussler, Leonid and Sippel, Martin and Kucukosman, Yakut Cansev and Buckingham, Sophia (2021) A Full-Scale Simulation and Analysis of Formation Flight during In-Air Capturing. In: Proceedings of the International Astronautical Congress, IAC. 72nd International Astronautical Congress (IAC), 25-29 Oct. 2021, Dubai, United Arab Emirates. ISSN 0074-1795. file

  Singh, Sunayna and Stappert, Sven and Bussler, Leonid and Sippel, Martin and Kucukosman, Yakut Cansev and Buckingham, Sophia (2022) Full-scale simulation and analysis of formation flight during in-air-capturing of a winged reusable launch vehicle. Journal of Space Safety Engineering, 9 (4), pp. 541-552. Elsevier. doi: 10.1016/j.jsse.2022.09.005. ISSN 2468-8967. Volltext nicht frei. file

  Sippel, Martin and Klevanski, Josef and van Foreest, Arnold and Gülhan, Ali and Esser, Burkard and Kuhn, Markus (2006) The SpaceLiner Concept and its Aerothermodynamic Challenges. 1st International ARA Days, 2006-07-03 - 2006-07-05, Archachon, France. Volltext nicht online.

  Sippel, Martin and Kopp, Alexander and Sinkó, Katalin and Mattsson, David (2012) Advanced Hypersonic Cryo-Tanks Research in CHATT. AIAA. 18th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 24.-28. Sep. 2012, Tours, France. ISBN 978-1-60086-931-0. file

  Sippel, Martin and Koschel, Wolfgang (2013) Raumfahrtantriebe 1 nach dem überarbeiteten und aktualisierten Vorlesungsskript von Univ. Prof. Dr.-Ing. Wolfgang Koschel, RWTH Aachen. DLR-Interner Bericht. SART TN-007/2012. Other. DLR. 163 S. Volltext nicht online.

  Sippel, Martin and Schwanekamp, Tobias and Bauer, Carola and Garbers, Nicole and van Foreest, Arnold and Tengzelius, Ulf and Lentsch, Aron (2012) Technical Maturation of the SpaceLiner Concept. American Institute of Aeronautics and Astronautics. 18th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Tours, Frankreich. ISBN 978-1-60086-931-0. file

  Sippel, Martin and Votta, Raffaele and Haya-Ramos, Rodrigo (2012) Advanced Launcher Technology Maturation Supported by EU-Aeronautic Research Projects. International Astronautical Federation. 63rd International Astronautical Congress 2012, 1.-5. Okt. 2012, Naples, Italy. file

  Sippel, Martin and Yamashiro, Ryoma (2012) Staged Combustion Cycle Rocket Engine Design Trade-Offs for Future Advanced Passenger Transport. Association Aéronautique et Astronautique. SPACE PROPULSION 2012,, 7.–10. Mai 2012, BORDEAUX, France. file

  Sippel, Martin (2009) Promising roadmap alternatives for the SpaceLiner. Acta Astronautica, 66, pp. 1652-1658. Elsevier. doi: 10.1016/j.actaastro.2010.01.020. ISSN ISSN 0094-5765. file

  Sippel, Martin (2009) SpaceLiner - a Visionary Concept of an Ultra Fast Passenger Transport under Investigation in FAST20XX. AIAA 2009, 14.-17. Sept. 2009, Pasadena, California. file

  Sippel, Martin (2009) Wiederverwendbare Boosterstufen für Ariane 5. Raumfahrt Concret, 56 (1/2009). Iniplu 2000. file

  Sippel, Martin (2008) Promising Roadmap Alternatives for the SpaceLiner. DLR-Interner Bericht, Project Report. Institute for spacesystems. (Unpublished) file

  Sippel, Martin (2007) Introducing the SpaceLiner Vision. 7th International Symposium on Launcher Technologies, 02.-05. April 2007, Barcelona, Spain. file

  Sippel, Martin (2014) Spaceliner – Reisen mit Raumfahrttechnologie. Luftfahrt der Zukunft, 08.12.2014, Braunschweig. (Unpublished) Volltext nicht online.

  Sippel, Martin (2015) SpaceLiner Development Roadmap and Technology&Research Requirements. DLR-Interner Bericht. SART TN-014/2014. Other. DLR. (Unpublished) Volltext nicht online.

  Sippel, Martin (2018) System Design of the SpaceLiner Project and Its Latest Technical Progress. The 20th AnnualMeeting of the China Association for Science and Technology, 26.5. - 27.5.2018, Hangzhou, China. file

  Sippel, Martin (2022) INTRODUCTION TO THE LS AND FALCON SYSTEMS DEFINITION AND REQUIREMENTS. VKI Lecture Series. Volltext nicht online.

  Sippel, Martin (2017) Point-to-Point Suborbital Passenger Transport with DLR SpaceLiner (Part 1 & 2). 9th International Association for the Advancement of Space Safety (IAASS) Conference, 18. - 20. October 2017, Toulouse, Frankreich. Volltext nicht online.

  Sippel, Martin (2021) Europe - Australia in 80 minutes: DLR-SpaceLiner vs. SpaceX Starship. London to Sydney in Five Hours: The Future of Aviation Conference, 29.-30.09.2021, London, England. Volltext nicht online.

  Sippel, Martin and Bussler, Leonid (2016) Abschätzung der Thermallasten am ATEK Flugdemonstrator. DLR-Interner Bericht. SART TN-008/2016. DLR. (Unpublished) Volltext nicht online.

  Sippel, Martin and Bussler, Leonid (2015) RLV-Referenzkonfigurationen des ATEK-Projektes ATEK-B02 – v1. DLR-Interner Bericht. SART TN-011/2015. Other. DLR. (Unpublished) Volltext nicht online.

  Sippel, Martin and Bussler, Leonid and Kopp, Alexander and Krummen, Sven and Valluchi, Cecilia and Wilken, Jascha (2017) Advanced Simulations of Reusable Hypersonic Rocket-Powered Stages. 21st AIAA International Space Planes and Hypersonics Technologies Conference, 6-9 March 2017, Xiamen, China. doi: 10.2514/6.2017-2170. file

  Sippel, Martin and Bussler, Leonid and Krause, Stefan and Cain, Sebastian and Stappert, Sven (2018) Bringing Highly Efficient RLV-Return Mode "In-Air-Capturing" to Reality. HiSST 2018, 26–29 November 2018, Moskau, Russland. file

  Sippel, Martin and Bussler, Leonid and Messe, Christian and Stappert, Sven and Schuster, Stephan (2020) Preliminary Analyses of Winged Reusable First Stages in Two- and Three-Stage to Orbit Configurations (RLVC4). Project Report. SART TN-015/2019. 106 S. Volltext nicht online.

  Sippel, Martin and Darkow, Nicolas and Fischer, Alexander and Wilken, Jascha and Reimer, Thomas and Rauh, Carolin and Thiele, Thomas (2019) Enhancing Critical RLV-technologies: Testing Reusable CryoTank Insulations. In: 70th International Astronautical Congress, IAC 2019. International Astronautical Congress (IAC) 2019, 21. – 25. October 2019, Washington D.C., USA. file

  Sippel, Martin and Dietlein, Ingrid (2010) Potential Early Applications of Advanced Effusion Cooled Ceramic Combustion Chambers. SPACE PROPULSION 2010, 3.–6. MAY 2010, SAN SEBASTIAN, SPAIN. file

  Sippel, Martin and Dietlein, Ingrid and David, Emmanuelle and Dumont, Etienne and Johannsson, Magni and Koch, Aaron (2013) Vergleichender technischer Überblick aktueller Konfigurationen von Raumfahrträgern. DLR-Interner Bericht. SART TN25-2013. DLR Bremen. (Unpublished) Volltext nicht online.

  Sippel, Martin and Dietlein, Ingrid and Hanowski, Nicolaus and Romberg, Oliver and Schubert, Daniel and Seboldt, Wolfgang and Weihs, Hendrik (2008) BERT - Bemannter europäischer Raumtransport / Studienzusammenfassung / SART-TN 007/2008. DLR-Interner Bericht. SART-TN 007/2008. DLR. (Unpublished) Volltext nicht online.

  Sippel, Martin and Dumont, Etienne and Clark, Vanessa and Koch, Aaron and David, Emmanuelle and Garbers, Nicole and Manfletti, C. and Höck, Birte and Geiss, Gunter (2014) Advanced Launcher Options under Constraints of Synergy, Commonality and Affordability. IAC 2014, 29.09.2014-03.10.2014, Toronto, Kanada. file

  Sippel, Martin and Dumont, Etienne and Dietlein, Ingrid (2011) Investigations of Future Expendable Launcher Options. 62nd International Astronautical Congress, Cape Town, SA., 03-07- Oktober 2011, Kapstadt, Süd Afrika. file

  Sippel, Martin and Dumont, Etienne and Trivailo, Olga and Koch, Aaron and Bussler, Leonid (2016) Feasibility of TSTO LOX-HC-Micro-Launcher operated from Europe Study on sensibility aspects for propulsion systems for ESA-ESTEC. DLR-Interner Bericht. SART TN-010/2015. Other. (Unpublished) Volltext nicht online.

  Sippel, Martin and Fahrenbach, Sarah (2019) Invited Lectures on SpaceLiner and related RLV-technologies. Lecture on SpaceLiner and related RLV-technologies, 30. - 31. Mai 2019, Beijing, China. Volltext nicht online.

  Sippel, Martin and Foreest, Arnold van (2010) SpaceLiner Rocket-Powered High-Speed Passenger Transportation Concept Evolving in FAST20XX. IAC 2010, 27. Sep- 01. Oktober, Prag, CZ. file

  Sippel, Martin and Klevanski, Josef (2005) Simulation of Dynamic Control Environments of the In-Air-Capturing Mechanism. 6th International Symposium on Launcher Technology, München, Deutschland. file

  Sippel, Martin and Klevanski, Josef and Steelant, Johan (2005) Comparative Study on Options for High-Speed Intercontinental Passenger Transports: Air-Breathing- vs. Rocket-Propelled. In: IAC-05-D2.4.09. IAC 2005, Fukuoka, Japan. file

  Sippel, Martin and Kopp, Alexander (2016) Progress on Advanced Cryo-Tanks Structural Design Achieved in CHATT-Project. 14th European Conference on Spacecraft Structures, Materials and Environmental Testing, 27.-30. Sept. 2016, Toulouse, France. file

  Sippel, Martin and Kopp, Alexander and Dietlein, Ingrid and Bock, M. and Stief, Malte and Fischer, Alexander and Darkow, Nicolas and Lentsch, A. and Mattsson, D. and Walton, C. and Zanchetta, M. and Krödel, M. and Schön, J. and Davidsson, P. and Dalenbring, M. and Freund, J. and Koussios, S. and Tapeinos, I. and Mahajan, A. and Hillewaert, K. and Sharifzadeh, S. and Sinko, K. (2016) Cryogenic hypersonic advanced tank Technologies Project final report. Project Report. ACP1-GA-2011-285117. DLR Bremen. 393 S. (Unpublished) Volltext nicht online.

  Sippel, Martin and Kopp, Alexander and Mattsson, David and Fraters, Arjan and Koussios, Sotiris (2013) Advanced Cryo-Tanks Research in CHATT. 5TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) 2013, 01.-05. Juli 2013, München, Deutschland. file

  Sippel, Martin and Kopp, Alexander and Mattsson, David and Koussios, Sotiris (2014) Advanced Cryo-Tanks Structural Design Investigated in CHATT. SSMET 2014, 01.04.2014-04.04.2014, Braunschweig. (In Press) file

  Sippel, Martin and Lang, Anna and Dumont, Etienne and Gerstmann, Jens and Montenegro, Sergio (2010) Advanced Technology Upper Stages for Future Launchers. IAC 2010, 27. Sep- 01. Oktober 2010, Prag, CZ. file

  Sippel, Martin and Okai, Keiichi and Kato, Hiromasa and Kumar, Apurva (2007) Preliminary Definition of a TBCC Propulsion System for a Mach 4.5 Supersonic Cruise Airliner. ISABE 2007, 02.-07. Sep 2007, Beijing, China. file

  Sippel, Martin and Schwanekamp, Tobias and Ortelt, Markus (2014) Staged Combustion Cycle Rocket Engine Subsystem Definition for Future Advanced Passenger Transport. Space Propulsion 2014, 19.5.2014-22.05.2014, Köln, Germany. file

  Sippel, Martin and Schwanekamp, Tobias and Trivailo, Olga and Lentsch, Aron (2013) Progress of SpaceLiner Rocket-Powered High-Speed Concept. 64th IAC, 23.09-27.09.2013, Bejing, China. file

  Sippel, Martin and Singh, Sunayna and Bussler, Leonid and Stappert, Sven and Buckingham, Sophia and Lopes, Silvania and Planquart, Philippe and Kucukosman, Yakut Cansev (2022) CFD analysis of interaction effects between vehicles in formation flight for in-air capturing of reusable launchers. International Astronautical Congress (IAC 2022), 18-22 September 2022, Paris, France. file

  Sippel, Martin and Singh, Sunayna and Stappert, Sven (2022) RLV-Return Mode “In-Air-Capturing” and Definition of its Development Roadmap. 9TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) 2022, 27. Juni - 01. Juli 2022, Lille, Frankreich. file

  Sippel, Martin and Stappert, Sven (2020) In-Air-Capturing Development Roadmap (State of the Art). Project Report. Deliverable D2.2. Other. European Commission (EC project number 821953). 52 S. file

  Sippel, Martin and Stappert, Sven (2019) Status of DLR investigations: „in-air-capturing“ history, interest for RLV, simulation & analyses. Kick-off Meeting FALCon Project, Bremen, Germany. file

  Sippel, Martin and Stappert, Sven and Bayrak, Yusuf Mete and Bussler, Leonid and Callsen, Steffen (2022) Systematic Assessment of SpaceLiner Passenger Cabin Emergency Separation Using Multi-Body Simulations. 2nd International Conference on High-Speed Vehicle Science Technology (HiSST), 11.-15. Sep. 2022, Brügge, Belgien. Volltext nicht online.

  Sippel, Martin and Stappert, Sven and Bussler, Leonid and Callsen, Steffen (2020) High-Performance, Partially Reusable Launchers for Europe. In: Proceedings of the International Astronautical Congress, IAC. 71st International Astronautical Congress (IAC 2020), 12.-14.10.2020, Cyberspace Edition. ISSN 0074-1795. file

  Sippel, Martin and Stappert, Sven and Bussler, Leonid and Dumont, Etienne (2017) Systematic Assessment of Reusable First-Stage Return Options. In: Proceedings of the International Astronautical Congress, IAC (D2.4.4). 68th International Astronautical Congress (IAC) 2017, 25.-29.09.2017, Adelaide, Australien. file

  Sippel, Martin and Stappert, Sven and Bussler, Leonid and Forbes-Spyratos, Sholto (2018) Technical Progress of Multiple-Mission Reusable Launch Vehicle SpaceLiner. HiSST 2018, 26–29 November 2018, Moskau, Russland. file

  Sippel, Martin and Stappert, Sven and Bussler, Leonid and Krause, Stefan and Cain, Sebastian and Espuch, Javier and Buckingham, Sophia and Penev, Valentin (2019) Highly Efficient RLV-Return Mode “In-Air-Capturing” Progressing by Preparation of Subscale Flight Tests. 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) 2019, 01-04. Juli 2019, Madrid, Spain. file

  Sippel, Martin and Stappert, Sven and Bussler, Leonid and Krause, Stefan and Cain, Sebastian and Espuch, Javier and Buckingham, Sophia and Penev, Vatentin (2019) Highly Efficient RLV-Return Mode “In-Air-Capturing” Progressing by Preparation of Subscale Flight Tests. 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) 2019, 01.-04. Juli 2019, Madrid, Spanien. file

  Sippel, Martin and Stappert, Sven and Bussler, Leonid and Messe, Christian (2019) Powerful & Flexible Future Launchers in 2- or 3-stage Configuration. International Astronautical Congress (IAC) 2019, 21. – 25. October 2019, Washington D.C., USA. file

  Sippel, Martin and Stappert, Sven and Bussler, Leonid and Messe, Christian (2019) Powerful & Flexible Future Launchers in 2- or 3-stage Configuration. In: 70th International Astronautical Congress, IAC 2019. 70th International Astronautical Congress, 21.-25.10.2019, Washington D.C., USA. file

  Sippel, Martin and Stappert, Sven and Bussler, Leonid and Singh, Sunayna and Krummen, Sven (2019) Ultra-Fast Passenger Transport Options Enabled by Reusable Launch Vehicles. Internationale Konferenz für Flugfahrzeuge, Aerothermodynamik und Wiedereintrittsmissionen und -technik (FAR), 30. Sept. - 03. Okt. 2019, Monopoli, Italien. file

  Sippel, Martin and Stappert, Sven and Callsen, Steffen and Bergmann, Kevin and Dietlein, Ingrid Monika and Bussler, Leonid (2022) Family of Launchers Approach vs. “Big-Size-Fits-All”. International Astronautical Congress (IAC 2022), 18-22 September 2022, Paris, France. file

  Sippel, Martin and Stappert, Sven and Callsen, Steffen and Dietlein, Ingrid and Bergmann, Kevin and Gülhan, Ali and Marquardt, Pascal and Lassmann, Jens and Hagemann, Gerald and Froebel, Ludger and Wolf, Marco and Plebuch, Alex (2021) A viable and sustainable European path into space – for cargo and astronauts. In: Proceedings of the International Astronautical Congress, IAC. 72nd International Astronautical Congress (IAC), 25.-29.10.2021, Dubai. ISSN 0074-1795. file

  Sippel, Martin and Stappert, Sven and Dietlein, Ingrid Monika and Merrem, Clemens Hans-Joachim and Wartemann, Viola and Rickmers, Peter and Bauer, Waldemar and Fuller, John (2020) Hypersonic Flight Experiment ReFEx: Status and Future Perspectives. In: Proceedings of the International Astronautical Congress, IAC. 71st International Astronautical Congress (IAC 2020), 12.-14.10.2020, Cyberspace Edition. ISSN 0074-1795. file

  Sippel, Martin and Stappert, Sven and Koch, Aaron (2018) Assessment of Multiple Mission Reusable Launch Vehicles. 69th International Astronautical Congress (IAC), 01.-05. Oktober 2018, Bremen, deutschland. file

  Sippel, Martin and Stappert, Sven and Koch, Aaron D. (2019) Assessment of multiple mission reusable launch vehicles. Journal of Space Safety Engineering (6), pp. 165-180. Elsevier. doi: 10.1016/j.jsse.2019.09.001. ISSN 2468-8967. Volltext nicht online.

  Sippel, Martin and Stappert, Sven and Pastrikakis, Vasileios and Barannik, Valentyn and Maksiuta, Dmytro and Moroz, Leonid (2022) Systematic Studies on Reusable Staged-Combustion Rocket Engine SLME for European Applications. 8th Space Propulsion 2022, 09.-13.05.2022, Estoril, Portugal. file

  Sippel, Martin and Stappert, Sven and Simioana, Madalin (2020) Technical Report on different RLV return modes’ Performances. Project Report. Deliverable D2.1. Other. European Commission (EC project number 821953). 111 S. file

  Sippel, Martin and Stappert, Sven and Singh, Sunayna (2022) In-Air-Capturing Development Roadmap (Update). Project Report. Deliverable D2.4. Other. 74 S. file

  Sippel, Martin and Stappert, Sven and Singh, Sunayna (2023) In-Air-Capturing Development Roadmap (Update). Project Report. Deliverable D2.4. 78 S. file

  Sippel, Martin and Stappert, Sven and Wilken, Jascha and Darkow, Nicolas and Cain, Sebastian and Krause, Stefan and Reimer, Thomas and Rauh, Carolin and Stefaniak, Daniel and Thiele, Thomas and Kronen, Rolf and Briese, Lale Evrim and Acquatella B., Paul and Schnepper, Klaus and Riccius, Joerg (2019) Focused research on RLV-technologies: the DLR project AKIRA. 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) 2019, 01.-04.07.2019, Madrid, Spanien. file

  Sippel, Martin and Trivailo, Olga and Bussler, Leonid and Lipp, Sarah and Valluchi, Cecilia (2016) Evolution of the SpaceLiner towards a Reusable TSTO-Launcher. International Astronautical Congress 2016, 26.-30. Sept 2016, Guadalajara, Mexico. file

  Sippel, Martin and Valluchi, Cecilia and Bussler, Leonid and Kopp, Alexander and Garbers, Nicole and Stappert, Sven and Krummen, Sven and Wilken, Jascha (2017) SpaceLiner Concept as Catalyst for Advanced Hypersonic Vehicles Research. 7TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) 2017, 03.-06.07.2017, Mailand, Italien. file

  Sippel, Martin and Weihs, Hendrik and Barth, Tarik (2009) Systematic Assessment of Advanced "Sharp-Edged" Lifting Body Re-entry Configurations. 60th International Astronautical Congress (IAC), Okt. 2009, Daejeon, Republic of Korea. Volltext nicht frei. file

  Sippel, Martin and Wilken, Jascha (2018) Preliminary Component Definition of Reusable Staged-Combustion Rocket Engine. Space Propulsion 2018, 14.-16.Mai 2018, Sevilla, Spanien. file

  Sippel, Martin and Yamashiro, Ryoma (2013) Preliminary Design Study of Main Rocket Engine for SpaceLiner High-Speed Passenger Transportation Concept. DLR-Interner Bericht. DLR Bremen; Jaxa Tsukuba, Japan. (Unpublished) file

  Sippel, Martin and van Foreest, Arnold (2007) Latest Progress in Research on the SpaceLiner High-Speed Passenger Transportation Concept. IAC 2007, 24.-28. September 2007, Hyderabad, India. file

  Sippel, Martin and van Foreest, Arnold and Dietlein, Ingrid and Schwanenkamp, Tobias and Kopp, Alexander and Neeb, Dominik (2011) System Analyses Driving Improved Aerothermodynamic Lay-out of the SpaceLiner Configuration. 7th ESA Aerothermodynamics Conference, 9.-12.5.2011, Brügge, Belgien. file

  Sippel, Martin and van Foreest, Arnold and Dutheil, Jean-Philippe and Philip, Peter (2007) Technical Assessments of Future European Space Transportation Options. Technical Assessments of Future European, 24.28. Sep 2007, Hyderabad, India. file

  Sippel, Martin and van Foreest, Arnold and Klevanski, Josef and Gerstmann, Jens and Dutheil, Jean-Philippe and Jäger, Markus and Philip, Peter (2008) Future European Expendable Launcher Options and Technology Preparation. In: IAC 2008. IAC 2008, 2008-09-29 - 2008-10-03, Glasgow, Großbritannien. file

  Sippel, Martin and van Foreest, Arnold and Klevanski, Josef and Gerstmann, Jens and Dutheil, Jean-Philippe and Jäger, Markus and Philip, Peter (2009) Future European Expendable Launcher Options and Technology Preparation. IAC, The International Astronautical Federation, 12.-16. Okt. 2009, Daejon, Korea. file

  Sippel, Martin and van Foreest, Arnold and Philip, Peter and Jäger, Markus (2009) Study Trade-Offs on Future European Expendable Launchers. 3RD EUROPEAN CONFERENCE FOR AEROSPACE SCIENCES (EUCASS), 11.-16. Okt. 2009, Versailles, France. file

  Stappert, Sven (2017) Simulation of the Separation Process of the SpaceLiner Booster from the SpaceLiner Passenger Stage. Project Report. SART TN-013/2017. 69 S. Volltext nicht online.

  Stappert, Sven (2018) Aerodynamics of the ACCD for the In-AirCapturing of the SpaceLiner Booster. Project Report. SART TN-016/2018. 35 S. Volltext nicht online.

  Stappert, Sven and Callsen, Steffen and Sippel, Martin (2022) Re-entry and Flight Dynamics of a Winged Reusable First Stage. In: 9th European Conference on Aeronautics and Space Sciences (EUCASS), 2022. 9th European Conference for Aeronatics and Space Sciences (EUCASS), 27.6.-01.07.2022, Lille, Frankreich. file

  Stappert, Sven and Dumont, Etienne (2016) Reusability of launcher vehicles by the method of SpaceX. Master's, DLR. Volltext nicht online.

  Stappert, Sven and Rickmers, Peter and Bauer, Waldemar and Sippel, Martin (2019) Mission Analysis and Preliminary Re-entry Trajectory Design of the DLR Reusability Flight Experiment ReFEx. 8th European Conference for Aeronautics and Space Sciences, 01.07.2019-04.07.2019, Madrid, Spanien. file

  Stappert, Sven and Sippel, Martin (2017) Critical Analysis of SpaceX Falcon 9 v1.2 Launcher and Missions. DLR-Interner Bericht. DLR SART TN-009/2017. Other. DLR. 61 S. (Unpublished) Volltext nicht online.

  Stappert, Sven and Sippel, Martin and Bussler, Leonid and Wilken, Jascha and Krummen, Sven (2018) SpaceLiner Cabin Escape System Design and Simulation of Emergency Separation from its Winged Stage. 22nd AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 17.Sep. - 19.Sep.2018, Orlando, Florida, USA. doi: 10.2514/6.2018-5255. file

  Stappert, Sven and Sippel, Martin and Callsen, Steffen and Bussler, Leonid (2022) Concept 4: A Reusable Heavy-Lift Winged Launch Vehicle using the In-Air-Capturing Method. 2nd International Conference on High-Speed Vehicle Science Technology (HiSST), 11.-15. Sep. 2022, Brügge, Belgien. file

  Stappert, Sven and Sippel, Martin and Kopp, Alexander and Thiele, Thomas and Kronen, Rolf and Marwege, Ansgar and Reimer, Thomas and Stefaniak, Daniel and Krause, Stefan and Cain, Sebastian and Riccius, Joerg and Bussler, Leonid and Darkow, Nicolas and Fischer, Alexander and Scheufler, Henning and Briese, Lale Evrim and Paul Acquatella, B. and Schnepper, Klaus and Beerhorst, Matthias and Vormschlag, Nele Marei (2018) DLR-Projekt AKIRA: Ausgewählte Kritische Technologien und Integrierte Systemuntersuchungen für RLV Anwendungen (Zwischenbericht). Project Report. SART TN-015/2018. 329 S. Volltext nicht online.

  Stappert, Sven and Stier, Annika (2019) Critical Analysis of the Falcon Heavy Launcher and its Maiden Flight. Project Report. SART-TN 004/2018. 51 S. Volltext nicht online.

  Stappert, Sven and Wilken, Jascha and Bussler, Leonid and Sippel, Martin (2019) A Systematic Comparison of Reusable First Stage Return Options. 8TH European Conference For Aeronautics and Space Sciences, 01.07.2019 - 04.07.2019, Madrid. file

  Stappert, Sven and Wilken, Jascha and Bussler, Leonid and Sippel, Martin (2019) A Systematic Assessment and Comparison of Reusable First Stage Return Options. In: Proceedings of the International Astronautical Congress, IAC. 70th International Astronautical Congress, 21.10. - 25.10.2019, Washington DC, DC, USA. file

  Stappert, Sven and Wilken, Jascha and Bussler, Leonid and Sippel, Martin (2020) AKIRA Bericht: Return Options. Project Report. SART TN-014/2019. 96 S. Volltext nicht online.

  Stappert, Sven and Wilken, Jascha and Bussler, Leonid and Sippel, Martin and Karl, Sebastian and Klevanski, Josef and Hantz, Christian and Briese, Lale Evrim and Schnepper, Klaus (2019) European Next Reusable Ariane (ENTRAIN): A Multidisciplinary Study on a VTVL and a VTHL Booster Stage. In: Proceedings of the International Astronautical Congress, IAC. 70th International Astronautical Congress, 21.10-25.10.2019, Washington DC. file

  Stappert, Sven and Wilken, Jascha and Calabuig, Guillermo Joaquin Dominguez and Sippel, Martin (2022) Evaluation of Parametric Cost Estimation in the Preliminary Design Phase of Reusable Launch Vehicles. In: 9th Conference on Aeronautics and Space Sciences (EUCASS), 2022. 9th European Conference on Aeronautics on Space Sciences (EUCASS), 27.06.-01.07.2022, Lille, Frankreich. file

  Stappert, Sven and Wilken, Jascha and Sippel, Martin and Dietlein, Ingrid Monika (2018) Evaluation of European Reusable VTVL Booster Stages. In: 2018 AIAA SPACE and Astronautics Forum and Exposition. 2018 AIAA SPACE and Astronautics Forum, 17.Sep. - 19.Sep. 2018, Orlando, Florida, USA. doi: 10.2514/6.2018-5239. file

  Stappert, Sven and Wilken, Jascha and Sippel, Martin and Dumont, Etienne (2018) Assessment of a European Reusable VTVL Booster Stage. Space Propulsion 2018, 14.5.-18.5.2018, Sevilla, Spanien. file

T

  Trivailo, Olga and Sippel, Martin and Lentsch, Aron and Sekercioglu , Ahmet (2013) Cost Modeling Considerations & Challenges of the SpaceLiner - An Advanced Hypersonic, Suborbital Spaceplane. In: AIAA SPACE 2013 Conference & Exposition. AIAA SPACE 2013 Conference & Exposition , 10-12 Sept 2013, San Diego. Volltext nicht frei. file

  Trivailo, Olga and Sippel, Martin and Şekercioğlu, Y. Ahmet (2012) Review of hardware cost estimation methods, models and tools applied to early phases of space mission planning. Progress in Aerospace Sciences. Elsevier. doi: 10.1016/j.paerosci.2012.02.001. Volltext nicht online.

  Trivailo, Olga (2015) Innovative Cost Engineering Approaches, Analyses and Methods Applied to SpaceLiner – an Advanced, Hypersonic, Suborbital Spaceplane Case-Study. Dissertation, Monash University, Melbourne, Australia. Volltext nicht online.

  Trovarelli, F. and Guidotti, G. and Medici, G. and Esser, B. and Schleutker, T. and Dietlein, I. and Gambacciani, G. and Governale, G. and Verant, J.-L. and Dauvois, Y. and Prevereaud, Y. (2021) Advanced European Re-Entry System Based on Inflatable Heat Shields EFESTO project overview: system and mission design and technology roadmap. International Astronautical Congress 2021, Dubai, United Arab Emirates. (Submitted) Volltext nicht online.

  Trovarelli, F. and Guidotti, Guiseppe and Medici, G. and Schleutker, Thorn and Dietlein, Ingrid Monika and Gambaccani, G. and Governale, Guiseppe and Verant, Jean-Luc and Dauvois, Y. and Prevereaud, Ysolde (2021) Advanced European Re-Entry System Based on Inflatable Heat Shields EFESTO project overview: system and mission design and technology roadmap. In: Proceedings of the International Astronautical Congress, IAC. International Astronautical Congress (IAC 2021), 25.-29.10.2021, Dubai, United Arab Emirates. ISSN 0074-1795. Volltext nicht frei. file

  Tröltzsch, Anke and Siggel, Martin and Kopp, Alexander and Schwanekamp, Tobias (2014) Multidisciplinary Analysis of the DLR SpaceLiner Concept by different Optimization Techniques. In: 5th European Conference on Computational Mechanics. International Center for Numerical Methods in Engineering. 11th World Congress on Computational Mechanics (WCCM XI), 20.-25. Juli 2014, Barcelona, Spanien. ISBN 978-84-942844-7-2. file

V

  Valluchi, Cecilia and Schwanekamp, Tobias and Bauer, Carola and Sippel, Martin and Wilken, Jascha (2016) SpaceLiner Cabin Escape System Integration. DLR-Interner Bericht. SART TN-020/2015. DLR. (Unpublished) Volltext nicht online.

  Valluchi, Cecilia and Sippel, Martin (2017) Hypersonic Morphing for the SpaceLiner Cabin Escape System. 7TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) 2017, 03.-06.07.2017, Mailand, Italien. file

  Valluci, Cecilia and Sippel, Martin and Dumont, Etienne and Wilken, Jascha (2017) Status Ariane 6 & Vega-C und Ariane Next Konzept. Project Report. SART TN-012/2016. Project thesis. 91 S. Volltext nicht online.

  Vormschlag, Nele Marei (2015) SpaceLiner Publikationen 2015. DLR-Interner Bericht. SART TN-012/2015. Other. DLR. (Unpublished) Volltext nicht online.

  Votta, Raffaele and Marini, Marco and Ranuzzi, Giuliano and Schlegat, Thomas and Hannemann, Klaus and Schwanekamp, Tobias and Sippel, Martin (2013) Rarefied Aerothermodynamics Technology Development for Future High-Altitude High-Speed Transport (EU-FAST20XX). AIAA SPACE 2013 Conference and Exposition, 10. - 12. Sept. 2013, San Diego, CA, USA. Volltext nicht online.

  Voß, Marcel (2013) Validierung der EcosimPro ESPSS Bibliothek STEADY anhand existierender Raketentriebwerke. DLR-Interner Bericht. SART TN008-2013. DLR. 28 S. (Unpublished) Volltext nicht online.

  van Foreest, Arnold (2010) Modeling of cryogenic sloshing including heat and mass transfer. AIAA Joint Propulsion Conference, 25.-28. juli 2010, Nashville, USA. file

  van Foreest, Arnold (2011) Report on trajectory analysis and optimization of the nominal flight trajectory and sensitivities. Project Report. SART-TN 006/2011. DLR. 25 S. (Unpublished) file

  van Foreest, Arnold and Dreyer, M. and Arndt, T. (2011) Moving Two-Fluid Systems Using the Volume-of-Fluid Method and Single-Temperature Approximation. AIAA Journal, 49 (12), pp. 2805-2813. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.J050482. ISSN 0001-1452. file

  van Foreest, Arnold (2014) Modeling of cryogenic sloshing including heat and mass transfer. Dissertation, Deutsches Zentrum für Luft- und Raumfahrt. Volltext nicht online.

  van Foreest, Arnold and Sippel, M. and Isselhorst, A. (2009) A fast engineering tool for simulation and design of propellant management systems in liquid propelled launcher stages. EUCASS 2009, 6.-9. juli 2009, Versaille, Frankreich. file

  van Foreest, Arnold and Sippel, Martin (2008) The Logistical Challenges of the SpaceLiner Concept. In: 1st International Academy of Astronautics Syposium on Private Human Access to Space. 1st International Academy of Astronautics Symposium on Private Human Access to Space, 2008-5-28-2008-5-30, Arcachon, Frankreich. file

  van Foreest, Arnold and Sippel, Martin and Gülhan, Ali and Esser, Burkard and Ambrosius, B.A.C. and Sudmeijer, K. (2009) transpiration cooling using liquid water. In: Journal of Thermophysics and Heat Transfer American Institute of Aeronautics and Astronautics. pp. 693-702. doi: 10.2514/1.39070. ISSN 0887-8722. file

  van Foreest, Arnold and Sippel, Martin and Klevanski, Josef and Gülhan, Ali and Esser, Burkard (2007) Transpiration Cooling to Handle the Aerothermodynamic Challenges of the SpaceLiner Concept. In: 2ND EUROPEAN CONFERENCE FOR AEROSPACE SCIENCES (EUCASS). 2ND EUROPEAN CONFERENCE FOR AEROSPACE SCIENCES (EUCASS), 2007-7-1-2007-7-6, Brussel, Belgien. file

  von Rüden, David (2020) Aerodynamic Coefficients of Lift-Generating Space Transportation Systems: Modeling and Simulation. Bachelor's. Volltext nicht online.

W

  Wilken, Jascha (2016) Sonic Boom Estimation: SALES. DLR-Interner Bericht. SART TN-013/2015. Other. DLR. 15 S. (Unpublished) Volltext nicht online.

  Wilken, Jascha (2017) SpaceLiner Subsystem Specification Document. DLR-Interner Bericht. SART TN-002/2017. DLR. 26 S. (Unpublished) Volltext nicht online.

  Wilken, Jascha (2017) MikroLauncher Konzept mit Geltreibstoffen. DLR-Interner Bericht. SART TN-008/2017. DLR. 12 S. (Unpublished) Volltext nicht online.

  Wilken, Jascha (2017) PMP 1.0. DLR-Interner Bericht. SART TN-003/2016. DLR. 20 S. (Unpublished) Volltext nicht online.

  Wilken, Jascha (2018) System Study of Slush Propellants for Future European Launch Vehicles. Space Propulsion 2018, 14.-18. Mai 2018, Sevilla, Spanien. file

  Wilken, Jascha and Bussler, Leonid and Forbes-Spyratos, Sholto (2018) SpaceLiner System Specification Document. Project Report. SART TN-003/2018. 61 S. Volltext nicht online.

  Wilken, Jascha and Callsen, Steffen and Daub, Dennis and Fischer, Alexander and Liebisch, Martin and Rauh, Carolin and Reimer, Thomas and Sippel, Martin (2022) Investigation of insulation and thermal protection systems for reusable cryogenic stages. 2nd International Conference on High-Speed Vehicle Science Technology, 11-15 September 2022, Bruges, Belgium. file

  Wilken, Jascha and Dietlein, Ingrid Monika and Sippel, Martin and Blanco Arnao, Gonzalo and Bonetti, Davide and Pontijas Fuentes, Irene and Recupero, Cristina and Cano Torres, Álvaro (2020) RESOLVE: Reference Mission Scenarios for Re-usable Launcher Concepts. Project Report. SART TN-003/2020. 42 S. Volltext nicht online.

  Wilken, Jascha and Dumont, Etienne and Stappert, Sven (2017) New features of tosca and rts in version 1.33. DLR-Interner Bericht. SART TN-003/2017. Institut für Raumfahrtssysteme. 22 S. (Unpublished) Volltext nicht online.

  Wilken, Jascha and Förster, Gero (2017) Modellierung des SpaceLiner TSTO Konzepts in PMP. DLR-Interner Bericht. SART TN-013/2016. DLR. 18 S. (Unpublished) Volltext nicht online.

  Wilken, Jascha and Sippel, Martin and Berger, Michael (2022) Critical Analysis of SpaceX's Next Generation Space Transportation System: Starship and Super Heavy. 2nd International Conference on High-Speed Vehicle Science Technology (HiSST), 11.-15. Sep. 2022, Brügge, Belgien. file

  Wilken, Jascha and Stappert, Sven (2019) Investigation of a European Reusable VTVL First Stage. 8th european conference for aeronautics and space sciences (eucass), 1 - 4 July 2019, Madrid, Spain. file

  Wilken, Jascha and Stappert, Sven and Bussler, Leonid and Sippel, Martin and Dumont, Etienne (2018) FUTURE EUROPEAN REUSABLE BOOSTER STAGES: EVALUATION OF VTHL AND VTVL RETURN METHODS. 69th International Astronautical Congress (IAC), 01.-05. Oktober 2018, Bremen, Deutschland. file

  Wisse, Menko and Obermaier, Georg and Dumont, Etienne and Ruwwe, Thomas (2011) VENUS - CONCEPTUAL DESIGN FOR VEGA NEW UPPER STAGE. 62nd International Astronautical Congress, 3.-7. Okt. 2011, Cape Town, South Africa. file

Y

  Yamashiro, Ryoma and Sippel, Martin (2012) PRELIMINARY DESIGN STUDY OF STAGED COMBUSTION CYCLE ROCKET ENGINE FOR SPACELINER HIGH-SPEED PASSENGER TRANSPORTATION CONCEPT. International Astronautical Federation. 63rd International Astronautical Congress 2012, 1.-5. Okt. 2012, Naples, Italy. file

Z

  Zilker, Franziska and Ecker, Tobias and Dumont, Etienne and Hannemann, Klaus (2017) Aerothermal Analysis of Reusable First Stage Launcher during Re-Entry Retro-Propulsion. 18. STAB-Workshop 2017, 07.-08. Nov. 2017, Göttingen, Deutschland. Volltext nicht online.

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