Items where Subject is "Institute of Space Propulsion"

Institutes and Facilities (141598)
- Institute of Space Propulsion (3192)
  - Allg. Kosten aufgr. Störfall- Verordnung (1)
  - Applied Hydrogen Technologies (34)
  - Chemical Propellant Technology (31)
  - Engineering (7)
  - Administrative Department & Staff (1)
  - Institut für Chemische Antriebe und Verfahrenstechnik (226)
  - Leitungsbereich RA (200)
  - Engineering (68)
  - Rocket Propulsion (821)
  - Rocket Engine Systems (100)
  - Rocket Propulsion Technology (151)
  - Spacecraft and Orbital Propulsion (101)
  - School-Lab LA (14)
  - Safety, Quality and Technical Services (8)
  - Technologie (289)
  - Propellants (346)
  - Test Facilities (87)

Number of items at this level: 869.

Accettura, A. and De Rose, L. and Bruno, C. and Koschel, W.Gonzales del Amo, J., and Caramelli, F. (2001) Advanced Propulsion Systems: Mission Scenarios, Critical Overview, and Key Technologies for New Demands. In: 37th Joint Propulsion Conference and Exhibit. 37th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Salt Lake City, Utah, 8 - 11 July 2001. Volltext nicht online.

Agrafiotis, Christos and Thomey, Dennis and de Oliveira, Lamark and Alkan, Gözde and Roeb, Martin and Sattler, Christian and Ebert, Miriam and Gobereit, Birgit (2022) A particle receiver-driven thermochemical cycle employing elemental sulphur for solar thermochemical energy storage: investigation of proppants as concentrated sunlight har-vesting media and sulphur trioxide splitting catalysts. Solar Energy, 234, pp. 21-38. Elsevier. doi: 10.1016/j.solener.2022.01.032. ISSN 0038-092X. Volltext nicht frei.

Agren, K. and Sippel, M. and Klevanski, J. (2004) Bahnsimulation von kritischen Flugsituationen und Havariefällen beim LFBB. Project Report. SART TN-011/2004. DLR. Volltext nicht online.

Aich, Ursula and Altgelt, Friederike and Alwast, Holger and Prof. Dr.-Ing. Arnhold, Thorsten and Askar, Enis and Bäcker, Maik and Bahrenberg, Karsten and Dr.-Ing. Bajohr, Siegfried and Beisswenger, Lucien and Benesch, Florian and Dr.-Ing. Beyer, Michael and Böhm, Tobias and Böttcher, John and Brunken, Gerrit and Dr. Burmeister, Frank and Dr.-Ing. Cao, Chen and Dr.-Ing. Chang, Chi Yao and Chikhi, Ilona and Chromik, Karsten and Demeusy, Tatiana and Depken, Jorgen Johannes and Deßloch, Christian and Dr. Dörner, Wolfgang and Dreizler, Urlich Walter and Drews, Dieter and Dr. Drexler, Andreas and Dyck, Alexander and Dr. Eckner, Ralf and Dr. Essler, Jürgen and Fahrenbach, Peter and Falkenroth, Achim and Fischer, Ute and Fliegener, Sascha and Dr. Flink, Christoph and Franz, Michael and Freund, Sebastian and Garcia-Lorenzana, Ignacio and Gerstenberg, Maik and Gess, Ronny and Dr. Götz, Michael and Hälbig, Jens and Hariri, Daniel and Hartisch, Torsten and Dr.-Ing. Heisterkamp, Beate and Herber, Michael and Dr.-Ing. Herbst, Sabrina and Dr. Heyn, Jürgen and Dr. Höcher, Thomas and Hoffmann, Jens and Hoke, Dennis and Mudhafar, Saif Husam and Dr. Jopen, Manuela and Prof. Dr. Jürgensen, Lars and Kahl, Manolo and Kalhammer, Philipp and Klipphardt, Heinrich and Kirchner, Frank and Klement, Jürgen and Knafl, Johannes and Knoop, Dominik and Kramer, Rainer and Krämer, Michael and Kreißig, Thomas and Kröll, Mirco and Prof. Dr. Krüger, Michael and Dr. Kurte, Roland and Lambertz, Uwe and Langenberg, Julius and Prof. Dr. Langenberg, Peter and Lehmann, Ingo and Lenz, Volker and Leunig, Andreas and Liebscher, Ulf and Linseisen, Bernhard and Lorenz, Carsten and Dr. Lotze, Martin and Lotze, Torsten and Ludwig, Roman and Dr. Mair, Georg and Mayer, Raphael and Dr.-Ing. Melcher, Berthold and Menke, Nina and Dr. Menzel, Jasmin and Marbecks, David A. and Metz, Christian and Dr. Meyer, Rüdiger and Dr. Monse, Susann and Mües, Suell and Neimann, Dimitri and Neumann, Holger and Pilz-Lansley, Alexander and Poga, Björn and Raisch, Matthias and Rathgeb, Daniel and Ravinel, Baptiste and Reinecke, Matthias and Dr.-Ing. Rhode, Michael and Saß, Frank and Schaldach, Gerd and Schallenberg, Daniel and Prof. Schenk, Joachim and Schenk, Marc and Schindzielarz, Kristin and Dr.-Ing. Schirrmeister, Steffen and Schmidt, Volker and Dr.-Ing. Schmidt, Dirk and Schmidt, Christoph and Dott.ssa Ing. Schmiedhofer, Silvia and Schraube, Christian and Schu, Reinhard and Schücker, Albert and Schuhmann, Kai-Uwe and Schwagereit, Martin and Schwalfenberg, Claudio and Schwendemann, Eckhard and Schymassek, Jan and Seiffert, Jörg and Dipl.-Ing. Sohn, Nicole and Stahl, David and Stange, Holger and Dr. Stehle, Simon and Steinbach, Olaf and Strauß, Andreas and Stypka, Sebastian and Tamaddony-Awal, Iman and Dr. Taube, Klaus and Dr.-Ing. Theiler, Géraldine and Dr.-Ing. Wackermann, Ken and Wehner, Michael and Weishaar, Christoph and Wichmann, Tolga and Wicker, Martin and Wiedemann, Martin and Wiegleb, Tobias and Prof. Dr. Wilke, Winfried and Winkler, Markus and Wolf, Claudia and Dr. Wunderlich, Lukas and Dr. Yilmaz, Hüseyin and Zeitzmann, Gunther and Ziegenbalg, Jürg and Ziegler, Alexandra and Zimmerling, Sebastian and Dr. Zinke, Gert (2024) Normungsroadmap Wasserstofftechnologien 2024. Project Report.

Albat, R. and Langel, G. and Haidn, O. (2007) Antriebssysteme. In: Handbuch der Raumfahrttechnik Handbuch der Raumfahrttechnik. Carl Hanser Verlag, München. ISBN 978-3-446-41185-2. Volltext nicht online.

Albers, L. and Knapp, B. (1995) Technische Marktanalyse von Heizoelbrennern ueber Verbrennungssysteme und Einspritzelemente im Leistungsbereich bis 1 MW (Studienarbeit). DLR-Interner Bericht. 645-95/12. DLR. 131 S. Volltext nicht online.

Alger, S. (2011) Micro-Hybrid-Thruster Test Campaign. Institutsseminarreihe, 2011-01-18, DLR Lampoldshausen, Germany. (Unpublished) Volltext nicht online.

Alting, J. (1998) Untersuchung der Stoß/Grenzschicht-Wechselwirkung in Entspannungsdüsen von Raketentriebwerken. DLR-Interner Bericht. 645-98/13. 146 S. Volltext nicht online.

Anoussaki, G. (1997) Image Processing using Khoros Application on Droplet-Tracking Velocimetry. DLR-Interner Bericht. 645-97/23. 56 S. Volltext nicht online.

Arnold, Richard (2008) Experimentelle Untersuchungen zur Filmkühlung in Raketenbrennkammern. Dissertation, Universität Stuttgart. Volltext nicht online.

Arnold, Richard and Suslov, Dmitry and Haidn, Oskar (2009) Influence Parameters on Film Cooling Effectiveness in a High Pressure Subscale Combustion Chamber. 47th AIAA Aerospace Sciences Meeting, 2009-01-05 - 2009-01-08, Orlando, FL, USA. Volltext nicht online.

Arnold, Richard and Suslov, Dmitry and Haidn, Oskar and Weigand, Bernhard (2008) Investigation of Film Cooling in a High Pressure LOX/GH2 Subscale Combustion Chamber. Space Propulsion 2008: 5th International Spacecraft Propulsion Conference & 2nd International Symposium on Propulsion for Space Transportation, 2008-05-05 - 2008-05-08, Heraklion, Crete, Greece. Volltext nicht online.

Arnold, R. and Santos, P. H. S. and deRidder, M. and Campanella, O. H. and Anderson, W. E. (2010) Comparison of Monomethylhydrazine/Hydroxypropylcellulose and Hydrocarbon/Silica Gels. 48th AIAA Aerospace Sciences Meeting, 2010-01-04 - 2010-01-07, Orlando, FL.

Arslan, S. and Herbertz, A. (2003) Modelle zur Vordimensionierung von Raketentriebwerks-Turbopumpen. Project Report, DLR-Interner Bericht. 647-2003/03. 62 S. Volltext nicht online.

Assenmacher, Oliver and Gelain, Riccardo and Rüttgers, Alexander and Petrarolo, Anna and Hendrick, Patrick (2024) Convolutional neural networks for image analysis of high-speed videos from two slab burners. Acta Astronautica (219), pp. 931-940. Elsevier. doi: 10.1016/j.actaastro.2024.04.005. ISSN 0094-5765.

Assovskiy, I. and Pein, R. (1999) Critical Phenomena in Catalytic Co Oxidation. In: Meeting of the Greek Section of the Combustion Institute. Second Meeting of the Greek Section of the Combustion Institute, Thessaloniki (gr), 26-27 November 1999. Volltext nicht online.

Ast, M. (1997) Droplet Tracking Velocimetry Dreifachbelichtung. DLR-Interner Bericht. 645-97/20. 33 S. Volltext nicht online.

Baier, R.-D.(1) and Broichhausen, K.-D.(1) and Koschel, W. (1997) Systematic Study on the Fluid Dynamical Behaviour of Streamwise and Laterally Inclined Jets in Crossflow. 42nd ASME Gas Turbine and Aeroengine Congress, Exposition and Users Symposium, Orlando, Florida, June 2-5, 1997. Volltext nicht online.

Bailey, S.C.C. and Haidn, O.J. and Martinuzzi, R.J. (1999) Investigation of Pressure Field Strukture and Vortex Shedding Suppression for Near-Wall Rectangular Cylinders. In: 13th ASCE Engineering Mechanics Division Conference. 13th ASCE Engineering Mechanics Conference, Baltimore MD, USA, June 13-16, 1999. Volltext nicht online.

Barsacq, M. (1997) Determination of Velocity Fields in a LOX/GH2-Rocket Model Combustor by Using the Droplet Tracking Velocimetry. DLR-Interner Bericht. 645-97/14. 34 S. Volltext nicht online.

Bartels, N. and Brändle, R. and Ciezki, H. and Feinauer, A. and Kampen von, J. and Liebl, H. and Pein, R. and Robers, A. and Schneider, G. and Woschnak, A. and Chernov, V. and Ernst, A. and Gany, A. and Natan, B. and Rahimi, S. and Shapira, A. and Solomon, Y. and Zaltzman, E. (2003) Final Report of the 1st Term of the Joint German-Israeli Basic Research Program for the Investigation of Metallized Gel Fuels and Propellants. DLR-Interner Bericht. DLR-IB 647-2003/14. 96 S. Volltext nicht online.

Bartels, N. and Brändle, R. and Ciezki, H. and Feinauer, A. and Liebl, J. and Kampen von, J. and Pein, R. and Robers, A. and Schneider, G. and Woschnak, A. (2002) Untersuchungen zum Fliess- und Versprühungsverhalten gelförmiger Brennstoffe. In: Symposium "Wirkung und Schutz, Explosivstoffe". Symposium "Wirkung und Schutz, Explosivstoffe", Mannheim, 5 - 7 November 2002. Volltext nicht online.

Bartels, N. and Kampen, J. von and Ciezki, H. and Begnini, M. (2003) The Atomization of Gelled Fuels with a Doublet Like-on-Like Impinging Jet Injector under Ambient Pressure and Temperature Conditions. In: International Workshop on Combustion and Propulsion, Lerici, La Spezia, Italy, 9-IWCP. Nineth International Workshop on Combustion and Propulsion, Lerici, La Spezia, Italy, September 14-18, 2003. Volltext nicht online.

Bartels, N. and Kampen von, J. and Ciezki, H. and Benigni, M. (2003) Investigation of the Spray Behavior of Gelled JetA-1/Aerosil-Mixtures with a Like-on-Like Impinging Jet Atomizer. In: Energetic Materials, Reactions of Propellants, Explosives and Pyrotechnics, 34, 37-1-37-11. ICT. 34th International Annual Conference of ICT, Karlsruhe, June 24 - June 27, 2003. Volltext nicht online.

Bauer, R. (1996) Modifizierung einer Sonden-Positioniereinrichtung zur automatisierten Kalibrierung von Fuenflochsonden. DLR-Interner Bericht. 645-96/18. 85 S. Volltext nicht online.

Bayer, M.F. (1995) Richtlinien zur Systematisierung von Arbeitsablaeufen waehrend der Qualifikationsphase eines Pruefstandes fuer Hochdruck-Raketentriebwerke. DLR-Interner Bericht. IB-645-95/11. DLR. 135 S. Volltext nicht online.

Bechle, M. (2004) Experimental assistance and data analysis of High Pressure LOX/H2 rocket engine combustion. DLR-Interner Bericht. 647-2004/11. Diploma. 111 S. Volltext nicht online.

Beck, P. and Wagner, Bernd and Haidn, O. (2017) The influence of secondary flows in the thrust acting on the axis of a radial LOx pump. In: 12th European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, ETC 2017. 12th European Conference on Turbomachinery Fluid Dynamics & Thermodynamics, 2017-04-03 - 2017-04-07, Stockholm, Sweden. doi: 10.29008/ETC2017-141. ISSN 2410-4833. Volltext nicht online.

Beer, S.(1) and Haidn, O.J. and Härle, H. (1995) Experimental Determination of the Evaporation Rate of Sprays. In: partec 95, pp. 423-432. 11th European Conference of ILASS-EUROPE on Atomization and Sprays, Nuernberg, March 21-23, 1995. Volltext nicht online.

Begnini, M. (2003) Investigation of the Spray Characteristics of the Gelled Fuel Jet A-1, using an Impinging Jet Atomizer. DLR-Interner Bericht. 647-2003/05. Diploma. 120 S. Volltext nicht online.

Beversdorff, M. and Clauß, W. and Förster, W. and Oschwald, M. and Waidmann, W. and Wojde, M. (1996) Temperatur (CARS) und Geschwindigkeitsmessungen (L2F) im Nachlauf einer Wasserstoff-Einblasflamme (TsAGI-Finne) in einer M=2 Ueberschallstroemung. DLR-Interner Bericht. 645-96/07. 66 S. Volltext nicht online.

Biehler, M. (2010) Untersuchungen und Bewertung von Designvarianten für Apogäumstriebwerke. Diploma, Universität Stuttgart. Volltext nicht online.

Bissinger, N. and Koschel, W. and Sacher, P. and Walther, R. (2000) SCRAM-Jet Investigations within the German Hypersonics Technology Program (1993-1996). In: Scramjet Propulsion Progress in Astronautics and Aeronautics, 189; pp. 119-158. AIAA. ISBN 1-56347-322-4. Volltext nicht online.

Blanc, A.(1) and Ciezki, H. and Feinauer, A. and Liehmann, W.(1) (1996) Spektroskopische Untersuchung an borhaltigen Festbrennstoffen in einer Staubbrennkammer. In: 27th International Annual Conference of ICT, Karlsruhe, F.R.G., June 25-28, 1996. Volltext nicht online.

Blanc, A.(1) and Ciezki, H.K. and Feinauer, A. and Liehmann, W.(1) (1997) Investigation of the Combustion Behaviour of Solid Fuels with Various Contents of Metal Particles in a Planar Step Combustor by IR-Spectroscopic Methods. In: 33rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Seattle, WA, July 6-9, 1997. Volltext nicht online.

Bobay, L. (2002) "Behavior of Particle Additives in the Turbulent Environment of a Solid Fuel Ramjet Combustion Chamber" and "Numerical Calculation of the Flow Behavior of Gelled Fuels in Impinging Jet Injector Nozzles". Project Report, DLR-Interner Bericht. 647-2002/08. 49 S. Volltext nicht online.

Boman, A. and Häggander, J. and Hass, J. (1999) Laser Welded Channel Wall Nozzle Design, Manufacturing and Hot Gas Testing. 35th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Los Angeles, CA, June 20-24, 1999. Volltext nicht online.

Boniface, Y. and Reeb, A. and Woodward, R. and Pal, S. and Mayer, W. and Santoro, R. (2000) Hot Fire Studies of LOX Primary Atomization from Rocket Engine Coaxial Injectors. In: Fourth International Symposium on Liquid Space Propulsion - Scientific Progress in the Service of Space Access at the Beginning of the Third Millennium -. 4th International Symosium on Space Propulsion, Heilbronn, March 13-15, 2000. Volltext nicht online.

Bonnent, J.-C. (1998) DTV programmes using Khoros new version. DLR-Interner Bericht. 645-98/11. 66 S. Volltext nicht online.

Bonnet, J.-C. (1998) Rapport d'activité. DLR-Interner Bericht. 645-98/09. 18 S. Volltext nicht online.

Bonnet, J.-Chr. (1997) DTV Programmes using Khoros. DLR-Interner Bericht. 645-97/30. 62 S. Volltext nicht online.

Boppana, Chaitanya Kumar (2021) A Spectroscopic Study of the OH* Radical and its Application in Thermometry. Master's, Delft University of Technology. Volltext nicht online.

Bouchardy, P. and Grisch, F. and Clauss, W. and Oschwald, M. and Stel'makh, O. and Smirnov, V. (1999) Joint CARS diagnostic test campaign on Mascotte and P8. In: Fifth French-German Colloquium Research on Liquid Rocket Propulsion. Fifth French-German Colloquium Research on Liquid Rocket Propulsion. Volltext nicht online.

Bouchardy, P. and Grisch, F. and Clauss, W. and Oschwald, M. and Stel'makh, O. and Smirnov, V. (2000) Joint CARS Measurements at MASCOTTE and P8. In: 6th French-German Colloquium on Research in Liquid Rocket Propulsion. 6th French-German Colloquium on Research into Liquid Rocket Propulsion Phenomena, Heidelberg, 09. - 11. Oktober 2000. Volltext nicht online.

Bouchez, M.(1) and Koschel, W. and Lepelletier, M.(2) and Lieberherr, J.F.(3) and Scherrer, D.(4) and Sylvestre, J.C.(5) (1996) Future Propulsion Concepts and Associated Technologies. In: 5th Symposium International, Paris, May 22-24, 1996. Volltext nicht online.

Bourauel, P. (2003) Auslegung eines Treibstofffördersystems für einen wiederverwendbaren Flüssigtreibstoffbooster. Project Report, DLR-Interner Bericht. 647-2003/12. 91 S. Volltext nicht online.

Branam, R. and Mayer, W. (2003) Characterisation of Cryogenic Injection at Supercritical Pressure. Journal of Propulsion and Power, 19 (3), pp. 342-355. Volltext nicht online.

Branam, R. and Schneider, G. and Volpp, A. and Mayer, W. (2002) Injection Characteristics on the Surface of a Coaxial Jet. In: AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, pp. 1-10. 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Indianapolis, IN, 8.-11. July 2002. Volltext nicht online.

Branam, R. and Telaar, J. and Hussong, J. and Mayer, W. (2001) Characterisation of Cryogenic Jets at Supercritical Conditions. In: Spray 2001. 6. Workshop über Techniken der Fluidzerstäubung und Untersuchungen von Sprühvorgängen, 6, II.4-1-II.4-8. Spray 2001. 6. Workshop über Techniken der Fluidzerstäubung und Untersuchungen von Sprühvorgängen, Hamburg-Harburg, 14. - 15. November 2001. ISBN 3-930400-46-1. Volltext nicht online.

Brummund, U. (2000) Experimental Studies of Compressible Mixing Layers. Project Report, DLR-Interner Bericht. 645-2000/14. 140 S. Volltext nicht online.

Brummund, U. and Berangere, M. (1999) A Comparative Study of Planar Mie and Rayleigh Scattering for Supersonic Flowfield Diagnostics. In: ICIASF 99, 42.1-42.10. ICIASF 99 18th International Congress on Instrumentation in Aerospace Simulation, Toulouse, France, June 14-17, 1999. Volltext nicht online.

Brummund, U. and Cessou, A. and Oschwald, M. and Vogel, and Grish, F. (1) and Bouchardy, P.(1) and Pealat, M. (1) and Vingert, L. (1) and Habiballah, M.(1) and Snyder, R. (2) and Herding, P. (2) and Scouflaire, P. (2) and Rolon, C. (2) and Candel, S. (2) (1995) Laser diagnostis for cryogenic propellant combustion studies. In: Proc.o the 2nd Int. Symposium on Liquid Rocket Prop.. Intern. Symposium on Liquid Rocket Prop. "Liquid Rocket Comb. Devices", Chtillon, June 19-21, 1995. Volltext nicht online.

Brummund, U. and Cessou, A. (1) and Haidn, O. and Oschwald, M. and Vogel, A. (1996) Characterization of a Cryogenic High Pressure Coaxial Injector Spray with Nonintrusive Optical Diagnostics. In: 12th Annual Conference of ILASS-Europe on Liquid Atomization and Spray Systems; Lund, SW, June 19-21, 1996, pp. 29-34. Volltext nicht online.

Brummund, U. and Cessou, A. (1) and Vogel, A. (1997) PLIF Imaging Measurements of a Co-Axial Rocket Injector Spray at Elevated Pressures. In: 26th Symposium (International) on Combustion, Naples, Italy, July 28 - Aug. 2, 1996. Volltext nicht online.

Brummund, U. and Cessou, A. (1) and Vogel, A. and Haidn, O. and Oschwald, M. (1996) Optische Diagnostik zur Charakterisierung von Treibstoffaufbereitung und Verbrennung in LO2/GH2- Modellbrennkammern. In: Deutscher Luft- und Raumfahrtkongreß, DGLR-Jahrestagung, Dresden, 24-27. September 1996, pp. 417-426. Volltext nicht online.

Brummund, U. and Cessou, A.(1) and Vogel, A. (1996) Experimental Studies on Atomization, Vaporization and Combustion for Liquid Rocket Propulsion. In: 20th Congress of the International Council of the Aeronautical Scienes, Sorrento, Italy, Sept. 8-13, 1996, pp. 1990-1995. Volltext nicht online.

Brummund, U. and Mesnier, B. (1999) Experimental Study of Compressible Mixing Layers. In: Fourteenth International Symposium on Air Breathing Engines. AIAA. 14th International Symposium on Airbreathing Engines, Florence, Sept. 5-10, 1999. ISBN 1-56347-357-7. Volltext nicht online.

Brummund, U. and Mesnier, B. (1999) Supersonic Combustion Testing with Laser Optical Diagnostics. In: ENERGETIC MATERIALS o Modeling of Phenomena o Experimental Characterization o Environmental Engineering, 26-1-26-14. 30th International Annual Conference (ICT), Karlsruhe (de), June 29 - July 2, 1999. Volltext nicht online.

Brummund, U. and Mesnier, B. (1998) Zweidimensionale Strömungs- und Verbrennungs-Diagnostik an einer Überschall-Brennkammer. In: Lasermethoden in der Strömungsmeßtechnik. 6. Fachtagung GALA, 40.1-40.6. Shaker Verlag GmbH, Postfach 1290, 52013 Aachen. 6. Fachtagung GALA, Essen, 28. - 30. September 1998. ISBN 3-8265-4287-8. Volltext nicht online.

Brummund, U. and Mesnier, B. (1998) Flow field visualization of non-reacting and reacting supersonic flows in a scramjet model combustor using non-intrusive optical diagnostics. In: 8th International Symposium on Flow Visualization, 1-4 September 1998, Sorrento, Italy. Volltext nicht online.

Brummund, U. and Nuding, J. (1997) Interaction of a compressible shear layer with shock waves: an experimental study. In: 35th AIAA Aerospace Sciences Meeting & Exhibit, Reno, NV, January 6-10, 1997. Volltext nicht online.

Brummund, U. and Waidmann, W. (1995) Planar Imaging Measurements in a Supersonic Ramjet Combustor using LIF and Laser Rayleigh Scattering. In: Proceedings Colloque Ecoulements Propulsifs dans les Systèmes de Transport Spatial, Vol. 1, pp. 291-293. Colloque Ecoulements Propulsifs dans les Systèmes de Transport Spatial, Bordeaux, 11-15 Sept. 1995; Poster. Volltext nicht online.

Brummund, U. and Waidmann, W. (1995) Two-Dimensional Lawer Induced Fluorescence and Rayleigh Scattering Flow Visualization of a Supersonic Ramjet Combustor. In: Euromech. Euromech Colloquium 335 "Image Techniques and Analysis in Fluid Dynamics", Rome 5-7 June, 1995. Volltext nicht online.

Brummund, U. and Waidmann, W. (1995) UV-Laser Spectroscopy Applied at a Supersonic Ramjet Combustor. In: In'Com Tagungsband. In'Com Tagungsband Heinrich Heine Universitaet, Duesseldorf, 20.24.03.95. Volltext nicht online.

Buddenberg, C. and Brumund, U. and Knapp, B. (1995) Laser induzierte Fluoreszenz (LIF) an einem Heizlbrenner mit Blauflammenverbrennung. DLR-Interner Bericht. 645-95/07. DLR. 25 S. Volltext nicht online.

Burkhardt, H. and Herbertz, A. and Sippel, M. and Klevanski, J. (2003) Solid Propellant Hypersonic X-Vehicle Options as RLV Technology Stepping Stones. In: DGLR Jahrbuch 2003, Band I, II und III. DGLR. Deutscher Luft- und Raumfahrtkongress, München, 17. - 20. November 2003. Volltext nicht online.

Burkhardt, H. and Sippel, M. and Herbertz, A. and Klevanski, J. (2002) Comparative Study of Kerosene and Methane Propellants for Reusable Liquid Boosters Stages. In: 4th International Conference on Launcher Technology "Space Launcher Liquid Propulsion". 4th International Conference on Launcher Technology "Space Launcher Liquid Propulsion", Liege, 3 - 6 December 2002. Volltext nicht online.

Burkhardt, H. and Sippel, M. and Herbertz, A. and Klevanski, J. (2004) Kerosene vs Methane: A Propellant Tradeoff for Reussable Liquid Booster Stages. Journal of Spacecraft and Rockets, 41 (5), pp. 762-769. Volltext nicht online.

Burkhardt, H. and Sippel, M. and Klevanski, J. (2004) ASSC-2 (Liquid Fly Back Booster with Ariane 5) System Requirements. DLR-Interner Bericht. 647-2004/05. 29 S. Volltext nicht online.

Burkhardt, H. and Sippel, M. and Klevanski, J. and Herbertz, A. (2002) Comparative Study of Kerosene and Methane Propellants for Reusable Liquid Boosters Stages. In: 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. AIAA. 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Indianapolis, IN, 7 - 10 July 2002. Volltext nicht online.

Burkhardt, H. and Sippel, M. and Krülle, G. and Janovsky, R. and Kassebom, M. and Lübberstedt, H. and Romberg, O. and Fritsche, B. HTG, Katlenburg-Lindau), (2002) Evaluation of Propulsion Systems for Satellite End-Of-Life De.Orbiting. In: AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, pp. 1-11. 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Indianapolis, IN, 7 - 10 July 2002. Volltext nicht online.

Burkhardt, H. and Herbertz, A. and Sippel, M. and Woschnak, A. and Riccius, J. (2004) Evaluation of Green Propellants for Space Application. DLR-Interner Bericht. 647-2004/03. 94 S.

Börner, Michael (2022) Stand und Perspektive der Fusionsforschung: Welchen Beitrag kann die Fusionsforschung perspektivisch zur Energieversorgung leisten? Space Forum Lampoldshausen, 2022-05-05, Lampoldshausen. Volltext nicht frei.

Candel, S. and Juniper, M. and Scoufflaire, P. and Rolon, C. and Clauss, W. and Klimenko, D. and Oschwald, M. and Grisch, F. and Bouchardy, P. and Vingert, L. V (2003) Investigation of subcritical and transcritical cryogenic combustion using imaging and laser techniques. In: International Symposium on Liquid Space Propulsion. 5th International Symposium on Liquid Space Propulsion, October 28 - 30, 2003, Chattanooga, TN. Volltext nicht online.

Carl, J. (1) and Fröhlke, K. and Haidn, J. and Weingartner, S. (1) (1996) Improved Combustion Efficiency of a H2/O2 Steam Generator for Spinning Reserve Applications. In: 11th World Hydrogen Energy Conference, Stuttgart, June 23-28, 1996, pp. 1418-1427. Volltext nicht online.

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Frey, M. and Hagemann, G. (1997) Kritische Betrachtung hoehenadaptiver Duesensysteme am Beispiel der Dualbell-Duese. In: Deutsche Gesellschft fuer Luft- und Raumfahrt, DGLR-Jahrestagung, Muenchen, Oktober 14-17, 1997. Volltext nicht online.

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Gross, A. and Haidn, O. and Stark, R. and Zeiss, W. and Weber, C. and Weiland, C. (2001) Experimental and Numerical Investigation of Heat Loads in Separated Nozzle Flow. In: 37th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. 37th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Salt Lake City, UT, 8 - 11. July 2001. Volltext nicht online.

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Génin, Chloé and Vieille, Bruno (2019) CNES/DLR cooperation for the preparation of future reusable launcher cryogenic engines. In: Proceedings of the 8th European Conference for Aeronautics and Space Sciences. 8th European Conference for Aeronautics and Space Sciences EUCASS, 2019-07-01 - 2019-07-04, Madrid, Spain. doi: 10.13009/EUCASS2019-825.

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Haberer, T. (1999) Laufzeitmessung von Druckpulsen in Röhren mit kleinem Innendurchmesser zur Bestimmung des Ansprechverhaltens pneumatischer Sonden. DLR-Interner Bericht. 645-99/02. Volltext nicht online.

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Haemisch, Jan and Suslov, Dmitry and Waxenegger-Wilfing, Günther and Dresia, Kai and Oschwald, Michael (2021) LUMEN - Design of the Regenerative Cooling System for an Expander Bleed Cycle Engine Using Methane. 7th International Space Propulsion Conference, 2021-03-17 - 2021-03-19, Virtual Conference.

Hagemann, G. (1996) High Pressure Reactive Heat Transfer Modelling. In: 2nd French-German Colloquium on Research on Liquid Rocket Propulsion, Aachen, May 30-31, 1996. Volltext nicht online.

Hagemann, G. (1997) Clustered Plug Nozzle Flowfield Simulations - ARPT WP 4100 -. DLR-Interner Bericht. 645-97/08. Volltext nicht online.

Hagemann, G. (1998) Clustered PLUG Nozzle Flowfield Simulations. ARPT WP 4100/4200/2460. DLR-Interner Bericht. 645-98/01. 62 S. Volltext nicht online.

Hagemann, G. (1998) ARPT-Thrust Chamber Flowfield Analysis. DLR-Interner Bericht. 645-98/08. 13 S. Volltext nicht online.

Hagemann, G. and Frey, M. (1996) Dual-Bell Nozzle Flowfield Simulations. DLR-Interner Bericht. 645-96/23. 66 S. Volltext nicht online.

Hagemann, G. and Frey, M. and Krülle, G. (1996) Hoehenadoption von Raketenduesen - das Potential zur Leistungsoptimierung von chemischen Antrieben. In: Deutscher Luft- und Raumfahrtkongress, DGLR-Jahrestagung, Dresden, 24.-27. September 1996. Volltext nicht online.

Hagemann, G. and Frey, M. and Manski, D. (1997) A Critical Assessment of Dual-Bell Nozzles. In: 33rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Seattle, WA, July 6-9, 1997. Volltext nicht online.

Hagemann, G. and Immich, H. and Nguyen, T. van and Dumnov, G. (1998) Advanced Rocket Nozzles. Journal of Propulsion and Power, 14 (5), pp. 620-633. Volltext nicht online.

Hagemann, G. and Immich, H. and Terhardt, M. (1998) Flow Phenomena in Advanced Rocket Nozzles - The Plug Nozzle. 34th AIAA/ASME/ASEE Joint Propulsion Conference & Exhibit, Cleveland, July 13-15. Volltext nicht online.

Hagemann, G. and Immich, H.(1) and Nguyen, van T.(2) and Dumnov,G.(3) (1) Daimler-Benz Aerospace, Muenchen, Germany, (1997) Advanced Rocket Nozzles. In: 3rd Intern.Symposium on Space Propulsion: From Launch to Space,Beijing, China, August 11-13, 1997. Volltext nicht online.

Hagemann, G. and Kleber, A. (1997) Design Approach for an Internal/External Expansion Plug Nozzle. DLR-Interner Bericht. 645-97/12. 28 S. Volltext nicht online.

Hagemann, G. and Krülle, G. (1995) Advanced Rocket Nozzle Flowfield Computations. In: Proceedings, pp. 767-776. Colloque Ecoulements Propulsifs dans les Systemes de Transport Spatial, Bordeaux 11-15 Sept. 1995. Volltext nicht online.

Hagemann, G. and Krülle, G. and Hannemann, K. (1996) Numerical Flowfield Analysis of the Next Generation Vulcan Nozzle. AIAA Journal of Propulsion and Power, Vol.12,No.4. Volltext nicht online.

Hagemann, G. and Krülle, G. and Hannemann, K.(1) (1995) Numerical Flowfield Analysis of the Next Generation Vulcan Nozzle. In: AIAA. 31st AIAA Joint Propulsion Conference and Exhibit July 10-12, 1995 / San Diego, CA. Volltext nicht online.

Hagemann, G. and Krülle, G. and Manski, D. (1995) Dual Expander Engine Flowfield Simulations. In: AIAA. 31st AIAA Joint Propulsion Conference and Exhibit, San Diego, July 10-12, 1995. Volltext nicht online.

Hagemann, G. and Manski, D. (1995) Dual-Expander Triebwerke - Analyse von Zyklus und Duesenstroemung eines innovativen Konzepts. In: DGLR-Jahrbuch. Deutscher Luft- und Raumfahrtkongreß 1995; DGLR-Jahrestagung Bonn, 26.-29. Sept. 1995. Volltext nicht online.

Hagemann, G. and Preuss, A. and Grauer, F. and Frey, M. and Kretschmer, J. and Ryden, R. and Jensen, K. and Stark, R. and Zerjeski, D. (2004) Flow Separation and Heat Transfer in High Area Ratio Nozzles. In: AIAA/ASME/SAE/ASEE Joint Propulsion Conference, pp. 1-8. 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Fort Lauderdale, FL, July 11-14, 2004. Volltext nicht online.

Hagemann, G. and Reijasse, P. (1998) Brief Review of Side-Load Models. Project Report, DLR-Interner Bericht. 645-98/23. Volltext nicht online.

Hagemann, G. and Rommel, T. and Schley, C. and Krülle, G. and Manski, D. (1995) Plug Nozzle Flowfield Calculations for SSTO Applications. In: AIAA. 31st AIAA Joint Propulsion Conference and Exhibit July 10-12, 1995/San Diego, CA. Volltext nicht online.

Hagemann, G. and Terhardt, M. and Frey, M. and Reijasse, P. and Onofri, M. and Nasuti, F. and Östlund, J. (2000) Flow Separation and Side-Loads in Rocket Nozzles. In: Fourth International Symposium on Liquid Space Propulsion - Scientific Progress in the Service of Space Access at the Beginning of the Third Millennium -. 4th International Symposium on Space Propulsion, Heilbronn, March 13-15, 2000. Volltext nicht online.

Hagemann, G. and Terhardt, M. and Haeseler, D. and Frey, M. (2000) Experimental and Analytical Design Verification of the Dual-Bell Concept. In: 36th Joint Propulsion Conference and Exhibit. 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Huntsville, AL, July 17-19, 2000. Volltext nicht online.

Hagemann, G. and Alting, J. and Kretschmer, J. and Terhardt, M. and Frey, M. and Ryden, R. and Stark, Ralf (2002) The Calorimeter Nozzle Programme. In: Proceedings of the 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. AIAA. 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 2002-07-07 - 2002-07-10, Indianapolis, USA. Volltext nicht online.

Haidn, O. (1999) European Propulsion Research and Development Beyond 2000. In: Eleventh Annual Symposium, The Pennsylvania State University. 11th Annual Symposium, University Park, Pennsylvania, PA, November 18-19, 1999. Volltext nicht online.

Haidn, O. (2004) Injection for Liquid Rocket Engines. In: ILASS-Europe 2004, pp. 1-7. The 19th Annual Conferne for Liquid Atomisation and Spray Systems, ILASS, Nottingham, 6-9 September 2004. Volltext nicht online.

Haidn, O. (1996) Current Activities in DLR LO2/GH2 Combustion Research. Vortrag beim Besuch der Pennstate University, College Park USA, July 1, 1996. Volltext nicht online.

Haidn, O. (2007) Innovationsklima im DLR - Von der Idee zum Prototypen. 8. Technologie-Transfer-Forum, 2007-11-29, Lampoldshausen, D. Volltext nicht online.

Haidn, O. (2007) Thrust Chamber - Related Research Activities at the Institute of Space Propulsion Lampoldshausen. 11th Research Institute, 2007-11-08, Xi'an, China. Volltext nicht online.

Haidn, O. and Beer, S.(1) (1995) Modeling of the Evaporation of a Subcooled Spray in Superheated Steam. In: Proc. Colloque coulements Propulsifs dans les Systmes de Transport Spatial, vol. 1, pp. 323-325. Colloque Ecoulements Propulsifs dans les Systmes de Transport Spatial, Bordeaux, 11. - 15. Sept. 1995; Poster. Volltext nicht online.

Haidn, O. and Greuel, D. and Herbertz, A. and Ortelt, M. and Hald, H. (2005) Application of Fiber Reinforced C/C Ceramic Structures in Liquid Rocket Engines. In: Space Challenges in XXI Century; Rocket Motors and Problems of Space Exploration Torus Press, Moscow. pp. 78-104. ISBN 5-94588-036-1. Volltext nicht online.

Haidn, O. and Habiballah, M. (2000) Research on High Pressure Cryogenic Combustion. In: Proceedings ODAS 2000, pp. 1-198. 2nd ONERA-DLR Aerospace Symposium (ODAS 2000), Berlin, June 15-16, 2000. Volltext nicht online.

Haidn, O. and Habiballah, M. (2003) Research on High Pressure Cryogenic Combustion. Aerospace Science Technology, 7 (6), pp. 473-491. Volltext nicht online.

Haidn, O. and Herbertz, A. and Greuel, D. and Ghadiani, S. and Ortelt, M. and Hald, H. (2003) Transpiration Cooling of Liquid Rocket Engines Applying Fiber-Reinforced C/C Structures. Space Challenge in 21st Century. 100 Years after the Tsiolkovskiy Idea on Space Missions Using Reactive Motors, "SPACE 03", Moscow-Kaluga, September 15-19, 2003. Volltext nicht online.

Haidn, O. and Oschwald, M. and Schäfer, K. and Suslov, D. (2007) Methane / Oxygen Activities at DLR Lampoldshausen. 7th CNES/DLR Launcher Symposium, 2007, Barcelone (Spain). Volltext nicht online.

Haidn, O. and Palkina, I. and Riccius, J. and Carregal-Ferreira, J. and Hansen, T. (2006) CFD-Simulation of M3 Micro Combustor Ignition (RCM-4) with ANSYS CFX. 3rd International Workshop on Rocket Combustion Modeling, 2006-03, Paris. Volltext nicht online.

Haidn, O. and Palkina, I. and Riccius, J. and Gernoth, A. (2007) Analysis of a Model Combustor Ignition and Comparison with Experimental Results. 43rd AIAA/ASME/ASEE Joint Propulsion Conference and Exhibit, 2007-07-08 - 2007-07-11, Cincinatti, OH (USA). Volltext nicht online.

Haidn, O. and Shatalov, O.P. and Tunik, Y.V. (2007) Laser-based ignition of hydrogen-oxygen mixtures. 20th ISSW, 2007, Göttingen (D). Volltext nicht online.

Haidn, O. and Shatalov, O.P. and Tunik, Y.V. (2007) Two models of hydrogen-oxygen mixture ignition as a result of a radiation impulse. 2nd European Conference on Aerospace Sciences EUCASS, 2007, Brusels (B). Volltext nicht online.

Haidn, O. and Stratmann, K. and Vuillermoz, P. (1) and Hermant, M. (2) and Popp, M. (3) (1995) P8 - The New French/German Research Test Facility for H2/O2-High Pressure Rocket Engine Combustion Devices. In: IAF. 46th Intern. Astronautical Federation Congress (IAF) Oct. 2-6, 1995, Oslo/Norway. Volltext nicht online.

Haidn, O. and Suslov, D. and Hald, H. and Ortelt, M. and Beyer, S. and Knab, O. (2007) Technology Development Towards an entirely CMC-based Combustion Chamber. 2nd European Conference on Aerospace Sciences EUCASS, Brussels (B). Volltext nicht online.

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Haidn, O.J. and Bailey, S.C.C. and Martinuzzi, R.J. (1999) Relating Pressure Field and Vortex Shedding Suppression for a Square Cylinder in the Vicinity of a Solid Wall. In: Turbulence and Shear Flow - 1, pp. 1039-1044. 1st Turbulence and Shear Flow Phenomena (TSFP), Santa Barbara, CA, Sept. 12-15, 1999. ISBN 1-56700-135-1. Volltext nicht online.

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Klevanski, J. and Sippel, M. and Herbertz, A. and Kauffmann, J. (2002) Innovatives Verfahren zum Bergen einer wiederverwendbaren, geflügelten Raumtransporterstufe. In: DGLR Jahrbuch 2002, pp. 1-10. Deutscher Luft- und Raumfahrtkongress, Stuttgart, 23. - 26. September 2002. Volltext nicht online.

Klevanski, Josef (2007) Research and Development of a Flight Control System for an Aeroelastic STS in the Preliminary Design Phase. In: 2ND EUROPEAN CONFERENCE FOR AEROSPACE SCIENCES (EUCASS). 2nd EUROPEAN CONFERENCE FOR AEROSPACE SCIENCES (EUCASS), 2007-07-01 - 2007-07-06, Brussels. Volltext nicht online.

Klevanski, Josef and Sippel, Martin (2005) Development of the Aeroelastic Mathematical Model of the STS as an Object of the Flight Control System in the Preliminary Design Phase. In: 6th International Symposium on Launcher Technologies. Flight Environment Control for Future and Operational Launchers. 6th International Symposium on Launcher Technologies, 2005-11-08 - 2005-11-11, Munich, Germany. Volltext nicht online.

Klevanski, Josef and Sippel, Martin and van Foreest, Arnold (2006) Steuerung periodischer Flugbahnen ("Skip"-Trajectories) von Luftfahrzeugen im Hyperschall. In: DGLR Jahrbuch 2006. Deutscher Luft- und Raumfahrtkongress 2006, 2006-11-06 - 2006-11-09, Braunschweig, Germany. Volltext nicht online.

Klimenko, D. (2003) Manual for Water CARS Program. DLR-Interner Bericht. 647-2003/18. 40 S. Volltext nicht online.

Klimenko, D. and Clauss, W. and Mayer, W. and Oschwald, M. and Smith, J. (2003) Optical Diagnostics and Instrumentation for Supercriticl Combustion Studies in a LOX/H2 Rocket Engine Combustion Chamber. In: International Congress on Instrumentation in Aerospace Simulation Facilities. 20th International Congress on Instrumentation in Aerospace Simulation Facilities, Göttingen, 19.-25. August 2003. Volltext nicht online.

Klimenko, D. and Clauss, W. and Oschwald, M. and Smith, J. and Mayer, W. (2002) CARS Temperature Mapping in a Cryogenic LOX-H2 Rocket Combustion Chamber under Supercritical Conditions. Journal of Raman Spectroscopy, 33, pp. 900-905. Volltext nicht online.

Klimenko, D. and Clauss, W. and Smith, J. and Mayer, W. and Oschwald, M. (2003) H2-CARS Thermoemtry in a Cryogenic LOX/GH2 Rocket Combustion Chamber under Supercritical Conditions. ONERA-DLR Meeting, Toulouse, March 26-27, 2003. Volltext nicht online.

Klimenko, D. and Clauss, W. and Smith, J. and Oschwald, M. (2004) CARS Spectroscopy at High Presssure in a Cryogenic LOX/H2-Rocket Combustion Chamber. In: 24th International Symposium on Space Technology and Science. 24th International Symposium on Space Technology and Science, Miyazaki, Japan, May 30 - June 6, 2004. Volltext nicht online.

Klimenko, D. and Smith, J. and Clauss, W. and Mayer, W. and Oschwald, M. (2003) H2-CARS Thermometry in a Cryogenic LOX/H2 Rocket Combustion Chamber under Supercritical Conditions. Space Challenge in 21st Century. 100 Years after the Tsiolkovskiy Idea on Space Missions Using Reactive Motors, "SPACE 03", Moscow-Kaluga, September 15-19, 2003. Volltext nicht online.

Klimov, V. (2002) Investigation of multiphase diffusion flame using a flat flame burner. DLR-Interner Bericht. 647-2002/11. 83 S. Volltext nicht online.

Klimov, V. and Ciezki, H. and Gemelli, E. (2003) Spectrocopic Investigation of the Multephase Diffusion Flame of an Aluminum Particle Laden Hydrogen Jet in a Hot Air Environment. In: Energetic Materials, Reactions of Propellants, Explosives and Pyrotechnics, ICT, 152-1-152-13. ICT. 34th International Annual Conference of ICT, Karlsruhe, June 24 - June 27, 2003. Volltext nicht online.

Knapp, B. and Buschulte, W. (1997) Der Raketenbrenner und seine Weiterentwicklung. Vortrag im "Haus der Technik", Essen, 11.-12. Juni 1997 -Moderne Hausheizungsbrenner und -anlagen-. Volltext nicht online.

Kobald, Mario (2014) Hybrid Rocket Propulsion. DLR Summer School 2014, 2014-07-28 - 2014-08-08, Lampoldshausen, Deutschland. (Unpublished) Volltext nicht online.

Kobald, Mario and Fischer, U. and Tomilin, K. and Schmierer, C. and Petrarolo, Anna (2017) Hybrid Sounding Rocket HEROS TRL 9. 7th European Conference for Aeronautics and Space Sciences (EUCASS), 2017-07-03 - 2017-07-06, Mailand, Italien. Volltext nicht online.

Kobald, Mario and Schmierer, C. and Ciezki, Helmut and Schlechtriem, S. and Toson, E. and De Luca, T. (2014) Evaluation of Paraffin-based Fuels for Hybrid Rocket Engines. In: 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and exhibit 2014. 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 2014-07-28 - 2014-07-30, Cleveland, USA. doi: 10.2514/6.2014-3646. Volltext nicht online.

Kobald, Mario and Verri, I. and Schlechtriem, S. (2014) Theoretical and Experimental Analysis of Liquid Layer Instability in Hybrid Rocket Engines. Space Propulsion 2014, 2014-05-18 - 2014-05-22, Köln, Deutschland. Volltext nicht frei.

Koch, A. (2001) Messung der Sauerstofftropfengrößen an einer Raketenmodellbrennkammer. DLR-Interner Bericht. 645-2001/04. Diploma. 120 S. Volltext nicht online.

Kodera, M. and Sunami, T. and Scheel, F. (2002) Numerical Study on the Supersonic Mixing Enhancement Using Streamwise Vortices. In: 11th AIAA/AAAF International Conferencse Space Planes and Hypersonic Sysems and Technologies. 11th AIAA/AAAF International Conference Space Planes and Hypersonic Sysems and Technologies, Orleans, France, 29 September - 4 October, 2002. Volltext nicht online.

Koschel, W. (1999) Selected Topics in Space Propulsion. In: Proceedings of The 3rd DLR-NAL Workshop, pp. 102-132. 3rd NAL-DLR Workshop, Tokyo, Japan; 9 - 15 January, 1999. Volltext nicht online.

Koschel, W. (1999) Technologies de pointe au DLR: Technologies pour les lanceurs. "Les Activités Spatiales en Allemagne"; 14 September 1999, Toulouse, France. Volltext nicht online.

Koschel, W. (1999) Europäische Strategie für Raumfahrtantriebe. Wissenschaftliches Kolloquium zum Thema "Raumfahrtantriebe der Zukunft - Vision und Wirklichkeit". Volltext nicht online.

Koschel, W. (1999) Luft- und Raumfahrtantriebe - Status und Perspektiven -. Technische Universität, München, 18. November 1999. Volltext nicht online.

Koschel, W. (1995) Hypersonic Educational Activities in German Universities. In: AIAA. 6th AIAA Intern. Aerospace Planes and Hypersonics Technology Conference, Chattanooga, April 3-7, 1995. Volltext nicht online.

Koschel, W. (1995) Dreidimensionale Temperaturfeldberechnung von gekuehlten Turbinenschaufeln mit beliebig gestalteter Innengeometrie. In: DGLR Fachausschußsitzung. "Experim. und numerische Simulation räumlicher Wärmeflüsse in gekühlten Bauteilen von Gasturbinen" TU Berlin, 27.-28.7.95. Volltext nicht online.

Koschel, W. (1996) Overview on Recent DLR Activities in the HDR-Program. In: 2nd French-German Colloquium on Research on Liquid Rocket Propulsion: Modelling of Liquid Rocket Combustion Phenomena, Aachen, May 30-31, 1996. Volltext nicht online.

Koschel, W. (1996) Airbreathing and Rocket Space Propulsion. 2nd NAL-DLR Workshop on Bilaterally Relevant Aerospace Activities, Koeln, March, 12-13, 1996. Volltext nicht online.

Koschel, W. (1996) Qualitaetssicherung und Systematisierung von Arbeitsablaeufen am Beispiel des europaeischen Forschungspruefstandes P8 fuer Hochdruckraketen im DLR Forschungszentrum Lampoldshausen. bei "Die Rolle des Qualitaetsmanagement im Forschungsunternehmen DLR", Koeln, May 2, 1996. Volltext nicht online.

Koschel, W. (1996) Technologische Anforderungen zukuenftiger Antriebe fuer Traegersysteme. Fakultaet fuer Luft- und Raumfahrttechnik der Universitaet Stuttgart, Stuttgart, Juni 13, 1996. Volltext nicht online.

Koschel, W. (1996) Current Status of Active Combustion Control - Combustion Kinetics -. AGARD-Workshop on Active Combustion Control for Propulsion Systems, Athens, Greece, May 6 - 9, 1996. Volltext nicht online.

Koschel, W. (1996) Basic Research in German Universities and DLR on High Speed Airbreathing Propulsion. In: AIAA 7th International Space Planes and Hypersonic Systems and Technologies Conference, Norfolk, VA, USA, November 18-22, 1996. Volltext nicht online.

Koschel, W. (1997) Raumfahrt - Nutzen heute und zukuenftig. Vortrag im Rahmen der Hochschultage Heilbronn, Fachhochschule Heilbronn, 10. Juni 1997. Volltext nicht online.

Koschel, W. (1997) Was treibt die Raumfahrt an? Vortrag anläßlich des Dialogs 1997, Köln-Porz, 11. Juni 1997. Volltext nicht online.

Koschel, W. (1998) Basic Hypersonic Propulsion Research in German Universities. In: AIAA 8th Intern. Space Planes and Hypersonic Systems. AIAA 8th International Space Planes and Hypersonic Systems , Norfolk, VA, April 27-30, 1998. Volltext nicht online.

Koschel, W. (1998) Design and Analysis of Scramjet Components. In: Von Karman Institute for Fluid Dynamics, Lecture Series 1998-01 High Speed Propulsion; January 26-29, 1998. Volltext nicht online.

Koschel, W. (1998) Engine Cycle Selection. In: Von Karman Institute for Fluid Dynamics, Lecture Series 1998-01 on High Speed Propulsion; January 26-29, 1998, Brussels. Volltext nicht online.

Koschel, W. (1998) Scramjet Performance Calculation and Testing. In: Von Karman Institute for Fluid Dynamics, Lecture Series 1998-01 High Speed Propulsion; January 26-29, 1998. Volltext nicht online.

Koschel, W. and Borghi, R.(1) (1997) French/German Research Program Results and Orientations. In: 3rd French/German Colloquium on Research on Liquid Rocket Propulsion, Marseille, France; June 5-6, 1997. Volltext nicht online.

Koschel, W. and Bussmann, J. (1998) Computation of High-Speed Reacting Flows in Air-breathing Nozzles. In: GAMM Annual Meeting 1998; Bremen, April 6-9, 1998, pp. 91-92. Jahrestagung 1998 der GAMM. Volltext nicht online.

Koschel, W. and Bußmann, J. and Sommerhäuser, J. (1) (1995) Chemically Reacting Non-Equilibrium Boundary Layers in Air Breathing Propulsion Systems. In: AIAA. 6th AIAA Intern. Aerospace Planes and Hypersonics Technology Conference, Chattanooga, April 3-7, 1995. Volltext nicht online.

Koschel, W. and Depolt, T.(1) (1996) EXTEND - An Approach for Knowledge Based Diagnostic System for Turbine Monitoring. 18th Symposium on Aircraft Integrated Monitoring Systems, University Stuttgart, Sept. 19-21, 1995. Volltext nicht online.

Koschel, W. and Falempin, F.(1) (1997) Combined rocket and airbreathing propulsion - European perspectives. In: 3rd International Symposium on Space Propulsion, August 11-13, 1997, Beijing, China. Volltext nicht online.

Koschel, W. and Haidn, J. and Krülle, G. (1996) P8 - The new French/German test facility for H2/O2-high pressure rocket engine combustion research. In: 11th World Hydrogen Energy Conference, Stuttgart, June 23-28, 1996, pp. 1815-1825. DECHEMA, Frankfurt, Germany. Volltext nicht online.

Koschel, W. and Haidn, O. and Krülle, G. (1996) Two-Phase Flow in Space Propulsion. In: XIXth International Congress on Theoretical and Applied Mechanics, Kyoto, Japan, Aug. 25-31, 1996. Volltext nicht online.

Koschel, W. and Haidn, O.J. (1998) P8 - The new French/German Test Facility for H2/O2 High Pressure Rocket Engine Combustion Research. International Journal of Hydrogen Energy, 23 (8), pp. 683-694. Volltext nicht online.

Koschel, W. and Heitmeier, F. (1) (1995) Ramjet and Scramjet Development Methodology for Hypersonic Launchers. In: Conference on Propulsion Flows in Space Transportation Systems, Bordeaux, Sept. 11-15, 1995, 548-. Bordeaux, Sept. 11-15, 1995. Volltext nicht online.

Koschel, W. and Heitmeier, F.(1) (1997) Test Facilities for Large Ramjets. In: AGARD-Conference on Future Aerospace Technology in the Service of the Alliance, Palaiseau, France, April 14-17, 1997. Volltext nicht online.

Koschel, W. and Heitmeier, F.(1) (1997) Test Facilities for Large Ramjets. In: AGARD Symposium on Future Aerospace Technology in the Service of the Alliance, 14 - 17 April, 1997, Palaiseau, France. Volltext nicht online.

Koschel, W. and Jürgens, B. (1999) Thermal Analysis of Fluid-Structural Interaction in High-Speed Engine Flow Fields. In: Fourteenth International Symposium on Air Breathing Engines. XIV ISABE, Florence, Italy; 5-10 September, 1999. ISBN 1-56347-357-7. Volltext nicht online.

Koschel, W. and Jürgens, B. (1998) Computation of High-Speed Engine Flow Fields with Multidimensional Solid Heat Conduction. In: GAMM Annual Meeting 1998; Bremen, April 6-9, 1998, pp. 89-90. Jahrestagung 1998 der GAMM. Volltext nicht online.

Koschel, W. and Kim, B.-S. (1999) Shape Optimization of a Front Suspension Fork According to the Axiom of Constant Stress. In: SAE-Conference and Exhibition. SAE-Conference and Exhibition, Detroit (us), March 1 - 4, 1999. Volltext nicht online.

Koschel, W. and Link, T. (1998) Computation of High-Speed Flows in Nonequilibrium. In: GAMM Annual Meeting 1998; April 6-9, 1998, pp. 47-48. Jahrestagung 1998 der GAMM. Volltext nicht online.

Koschel, W. and Link, T. and Fox, U. (1998) Computation of Hypersonic Propulsion System Expansion Flows Considering Hydrogen/Air High Temperature Effects. In: AIAA 8th Intern. Space Planes and Hypersonic Systems and Technologies Conference, April 27-30, 1998, Norfolk, VA. Volltext nicht online.

Koschel, W. and Link, T.(1) and Fox, U.(1) (1997) Computation of High-Speed Reacting Flows Using a Finite Element Method. In: GAMM Annual Meeting 1997; March 24-27, 1997, Regensburg, Germany, pp. 35-36. Volltext nicht online.

Koschel, W. and Novelli, Ph. (1999) JAPHAR - A joint ONERA-DLR research project on high speed airbreathing propulsion. In: Fourteenth International Symposium on Air Breathing Engines. AIAA. XIV ISABE, Florence, Italy; 5-10 September, 1999. ISBN 1-56347-357-7. Volltext nicht online.

Koschel, W. and Parvizinia, M.(1) and Baier, R.-D.(2) and Broichhausen, K.-D.(2) (1997) Numerical and Experimental Study on the Influence of Angle Orientations on the Behaviour of Discrete Film Cooling Holes on Turbine Bladings. In: 13th International Symposium on Air Breathing Engines, ISABE, Chattanooga, TE, Sept. 7-12, 1997, 1, pp. 758-768. Volltext nicht online.

Koschel, W. and Saßnick, H.-D. and Janovsky, R.(1) and Koppenwallner, G.(2) and Kovaltschuk, V. (3) (1996) Integrated Measurement System for a Hypersonic Experimental Vehicle. In: 47th International Astronautical Congress, Beijing, China, Oct. 7-11, 1996. Volltext nicht online.

Koschel, W. and Schneider, A. (1999) Detailed analysis of a mixed compression hypersonic intake. In: Fourteenth International Symposium on Air Breathing Engines. AIAA. XIV ISABE, Florence, Italy; 5-10 September, 1999. ISBN 1-56347-357-7. Volltext nicht online.

Koschel, W. and Tölle, K.-H. (1) (1995) Methoden und Verfahren zur Auslegung einer aktiv gekuehlten Duesenstruktur nach der statischen Aerothermo- elastizitaetstheorie. In: Jahrbuch 1995, DGLR, pp. 303-312. Deutscher Luft- und Raumfahrtkongreß; DGLR-Jahrestagung, Bonn, 26.-29. Sept. 1995. Volltext nicht online.

Koschel, W. and Vuillermoz, P. (1998) Research on Liquid Rocket Propulsion. In: Research on Liquid Rocket Propulsion, 4th. Fourth French - German Colloquium. Volltext nicht online.

Koschel, W. and Walther, R.(1) and Sabelnikov, V.(2) and Korontsvit, Y.(2) and Ivanov, V.(2) (1997) Investigations into the Aerothermodynamic Characteristics of Scramjet Components. In: 13th International Symposium on Air Breathing Engines,ISABE, Chattanooga, TE, Sept. 7-12, 1997, 1, pp. 598-606. Volltext nicht online.

Koschel, W. and van Keuk, J. and Ballmann, J. and Schneider, A. (1998) Numerical Simulation of Hypersonic Inlet Flows. In: AIAA 8th Intern. Space Planes and Hypersonic Systems and Technologies Conference, April 27-30, 1998, Norfolk, VA. Volltext nicht online.

Koschel, W.W. and Haidn, O.J. (1997) Spray '97 / 3. Workshop über Sprays, Erfassung von Sprühvorgängen und Techniken der Fluidzerstäubung. In: 3. Workshop über Sprays, Erfassung von Sprühvorgängen und Techniken der Fluidzerstäubung, 3. Spray '97, Lampoldshausen (de), 22.-23. Oktober 1997. ISBN 3-89100-029-4. Volltext nicht online.

Kronmüller, H. (2000) Stationäre numerische Strömungssimulationen mit AeroShape-3D zum Kerndiffusor am P8. DLR-Interner Bericht. 645-2000/10. 56 S. Volltext nicht online.

Kronmüller, Harald (1999) Bestimmung des transienten heißgas- und kühlmittelseitigen Wärmeübergangs einer Hochdruck-Raketenbrennkammer auf Basis der inversen Formulierung der Fourier'schen Wärmeleitgleichung. DLR-Interner Bericht. 645-99/03. Diploma. Volltext nicht online.

Kronmüller, H. and Schäfer, K. and Stark, R. and Zimmermann, H. (2002) Kaltgas-Höhensimulationsprüfstand P6.2 des DLR Lampoldshausen. In: DGLR Jahrbuch 2002, III. DGLR. Deutscher Luft- und Raumfahrtkongress, 2002-09-23 - 2002-09-26, Stuttgart, Deutschland.

Kronmüller, H. and Schäfer, K. and Zimmermann, H. and Stark, R. (2002) Cold Gas Subscale Test Facility P6.2 at DLR Lampoldshausen. In: International Symposium on Propulsion for Space Transportation of the XXIst century, pp. 1-8. 6th International Symposium on Propulsion for Space Transportation of the XXI century, Palais des Congress, Versailles, France, 14 - 17 May 2002, 2002-05-14 - 2002-05-17, Versailles, France.

Krämer, H. (1996) Programmierung eines Messdatenerfassungs- und Auswerteprogramms zur Untersuchung von Brennluftstroemungen in Heizoelbrennersystemen. DLR-Interner Bericht. 645-96/14. 67 S. Volltext nicht online.

Krühsel, G. and Schäfer, K. (2001) Design and Development of an Ethanol/LOX Injection Head for Rocket Steam Generator (45 kg/s Steam) and Experimental Study of Combustion Stability. In: Fourth International Conference on Green Propellants for Space Propulsion. 4th International Conference on Green Propulsion for Space Propulsion, Noordwijk, The Netherlands, 20-22 June 2001. Volltext nicht online.

Krühsel, G. and Schäfer, K. (2003) Design, Development Evolution of an Ethanol/LOX Injection Head for Rocket Steam Generator of High Flowrate. In: 39th Joint Propulsion Conference and Exhibit. AIAA. 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Huntsville, AL, 20 - 23 July 2003. Volltext nicht online.

Krülle, G. and Golovitchev, V.(1) and Schley, C.-A. and Hagemann, G. (1995) Turbulence Modeling in High Pressure H2/O2 Rocket Engines. 10th Symposium on Turbulent Shear Flows Pennsylvania State University, August 14-16, 1995. Volltext nicht online.

Krülle, G. and Mayer, W. (1996) DLR-Activities in Physical and Chemical Modelling. In: 2nd French-German Colloquium on Research on Liquid Rocket Propulsion: Modelling of Liquid Rocket Combustion Phenomena, Aachen, May 30-31, 1996. Volltext nicht online.

Krülle, G. and Schley, C.-A. (1995) Fluid Injection Process in High Pressure H2/O2 Rocket Engines: derived models and numerical simulations. 11th European Conference of ILASS on Atomization and Sprays, Nuernberg, 21-23.03.1995. Volltext nicht online.

Krülle, G. and Schley, C.-A. (1996) Brennraummodellierung von chemischen Hochleistungs- Raketenantrieben im Rahmen des DLR-Projektes Hochdruckverbrennung fuer Raketenantriebe HDR. In: Deutscher Luft- und Raumfahrtkongress, DGLR-Jahrestagung Dresden, 24-27. September 1996. Volltext nicht online.

Kuentzmann, P. (1) and Vuillermoz, P. (2) and Krülle, G. (1996) Numerical Simulation of Propulsion Systems. In: 5th International Symposium on "Propulsion in Spatial Transports", Paris, May 22-24, 1996. Volltext nicht online.

Kuhl, D. (1998) Thermomechanical Analysis of Rocket Combustion Chamber. In: Fourth World Congress on Computational Mechanics (Abstracts). Fourth World Congress on Computational Mechanics, Buenos Aires, Argentina, 29 June - 2 July, 1998. Volltext nicht online.

Kuhl, D. (1996) Robuste Zeitintegration in der nichtlinearen Elastodynamik. Institut für Baumechanik und Numerische Mechanik, Universitaet Hannover / DFG Forschergruppe, Hannover, 19. Juni 1996. Volltext nicht online.

Kuhl, D. and Crisfield, M.A. (1999) Energy-Conserving and Decaying Algorithms in Non-Linear Structural Dynamics. International Journal for Numerical Methods in Engineering, 45, pp. 569-599. Volltext nicht online.

Kuhl, D. and Fröhlke, K. and Haidn, O. (1998) Analysis of Hydrogen/Oxygen Combustor Heat Transfer and Structural Failure. In: HYDROGEN ENERGY PROGRESS XII Proceedings of the 12th World Hydrogen Energy Conference. Asociacion Argentina del Hidrogeno. 12th World Hydrogen Energy Conference, Buenos Aires, Argentinia, 21. - 26. June 1998. ISBN 987-97075-0-8. Volltext nicht online.

Kuhl, D. and Haidn, O.J. and Josien, N. and Coutellier, D. (1998) Structural Optimization of Rocket Engine Cooling Channels. In: 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conf. & Exhibit, July 13-15, 1998, Cleveland, OH. Volltext nicht online.

Kuhl, D. and Holzer, A. and Haidn, J. (1999) Computational Solution of the Inverse Heat Conduction Problem of Rocket Combustion Chambers. 35th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Los Angeles, CA, June 20-23, 1999. Volltext nicht online.

Kuhl, D. and Ramm, E. (1998) Generalized Energy-Momentum Method for Non-linear Dynamics of Shells. In: Fourth World Congress on Computational Mechanics (Abstracts). Fourth World Congress on Computational Mechanics, Buenos Aires, Argentina, 29 June - 2 July, 1998. Volltext nicht online.

Kuhl, D. and Ramm, E. (1) (1996) Conservation of Energy and Momentum for Implicit Single Step Time Integration Schemes. In: Proceedings of the 3rd European Conference on Structural Dynamics: EURODYN '96, Florence, Italy June 5-8, 1996, pp. 349-356. Volltext nicht online.

Kuhl, D. and Riccius, J. and Haidn, O. (2000) Thermomechanical Fluid-Structure Analysis and Mathematical Optimization Techniques Applied to Cryogenic Liquid Rocket Engine Design. In: Fourth International Symposium on Liquid Space Propulsion - Scientific Progress in the Service of Space Access at the Beginning of the Third Millennium -. 4th International Symosium on Space Propulsion, Heilbronn, March 13-15, 2000. Volltext nicht online.

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Kuhl, D. and Woschnak, A. and Haidn, O.J. (1998) Coupled Heat Transfer and Stress Analysis of Rocket Combustion Chambers. 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Cleveland, OH, July 13-15, 1998. Volltext nicht online.

Kwan, W. and Frey, M. (1999) Clustered and Axisymmetric Plug Nozzle Flowfield Simulations - ARPT WP 6300. Project Report, DLR-Interner Bericht. 645-1999/16. 51 S. Volltext nicht online.

Kwan, W. and Stark, R. (2002) Flow Separation Phenomena in Subscale Rocket Nozzles. In: AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, pp. 1-9. 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Indianapolis, IN, 7 - 10 July 2002. Volltext nicht online.

Larch, S. (1998) Experimente zur Effusionskühlung in Raketenbrennkammern und ihre Auswirkung auf die Wandtemperatur. DLR-Interner Bericht. 645-98/30. Diploma. Volltext nicht online.

Lauck, Felix and Balkenhohl, Jakob and Negri, Michele and Freudenmann, Dominic and Schlechtriem, Stefan (2020) Green bipropellant development – A study on the hypergolicity of imidazole thiocyanate ionic liquids with hydrogen peroxide in an automated drop test setup. Combustion and Flame, 226, pp. 87-97. Elsevier. doi: 10.1016/j.combustflame.2020.11.033. ISSN 0010-2180.

Lauck, Felix and Freudenmann, Dominic (2023) Hydrogen Peroxide Research Activities at DLR Lampoldshausen. Innovative Propulsion Workshop, 2023-06-28 - 2023-06-30, Noordwijk, Niederlande. Volltext nicht frei.

Lauck, Felix and Negri, Michele and Freudenmann, Dominic and Schlechtriem, S. (2020) Selection of Ionic Liquids and Characterization of Hypergolicy with Hydrogen Peroxide. International Journal of Energetic Materials and Chemical Propulsion, 19 (1), pp. 25-37. Begell House. doi: 10.1615/IntJEnergeticMaterialsChemProp.2019028004. ISSN 2150-766X.

Lauck, Felix and Negri, Michele and Freudenmann, Dominic and Schlechtriem, Stefan (2019) Study on hypergolic ignition of ionic liquid solutions. In: Proceedings of the 8th European Conference for Aeronautics and Space Sciences. 8th European Conference for Aeronautics and Space Sciences EUCASS, 2019-07-01 - 2019-07-04, Madrid, Spain. doi: 10.13009/EUCASS2019-653.

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Lauck, Felix and Witte, Jan and Werling, Lukas and Schlechtriem, S. (2024) Lessons learned from the development and testing of the novel green hypergolic propellant HIP_11. 9th edition of the Space Propulsion Conference 2024, 2024-05-20 - 2024-05-23, Glasgow. Volltext nicht frei.

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Mayer, W. and Schik, A. (1998) Atomization and Breakup of Cryogenic Propellants Under High-Pressure Subcritical and Supercritical Conditions. Journal of Propulsion and Power, 14 (5), pp. 835-842. Volltext nicht online.

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Mayer, W. and Schik, A. and Ivancic, B. and Krülle, G. (1997) Atomization and Combustion of Cryogenic Liquids at High Pressures. In: 13th Annual Conference on Liquid and Atomization and Spray Systems, Florence, Italy, July 9-11, 1997, pp. 179-188. Volltext nicht online.

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Schmidt, S. (1999) Experimentelle Untersuchung zur Strömungsablösung in überexpandierten Raketendüsen. DLR-Interner Bericht. 645-1999/11. Diploma. 81 S. Volltext nicht online.

Schmidt, S. (1997) Untersuchung ueber den Einfluss von Fertigungstoleranzen auf das Kalibrierkennfeld einer pneumatischen Fuenfloch-Sonde. DLR-Interner Bericht. L-IB 645-97/07. 37 S. Volltext nicht online.

Schmidt, V. (1996) Visualisierung und Dichtebestimmung von kompressiblen Stroemungen mit Hilfe von Rayleighstreuung. DLR-Interner Bericht. 645-96/19. 65 S. Volltext nicht online.

Schmidt, V. and Ciezki, H. (2003) Schlieren and OH Emission Visualization of the Primary Ignition Process of a Coaxial lGH2/LOX Spray. In: 7th Triennial International Symposium on Fluid Control, Measurement and Visualization FLUCOME'03. 7th Triennial International Symposium on Fluid Control, Measurement and Visualization FLUCOME'03, Sorrento, Italy, August 25-28, 2003. ISBN 0-9533991-4-1. Volltext nicht online.

Schmidt, V. and Gurliat, O. and Oschwald, M. and Haidn, O. (2002) Influence of J and We Number on GH2/LOX Ignition Process. In: ILASS-Europe 2002. ILASS-Europe 2002, Zaragoza, 9. - 11. September 2002. Volltext nicht online.

Schmidt, V. and McConalogue, B. and Sender, J. and Oschwald, M. (2000) Simultaneous Observation of Liquid Phase Distribution and Flame Front Evolution during the Ignition Transcient of a LOX/GH2-Combustor. In: 9th International Symposium on Flow Visualization, 271-1-271-7. 9th International Symposium on Flow Visualization, Edinburgh, Scotland, August 22-25, 2000. Volltext nicht online.

Schmidt, V. and Puck, T. and Stein, C. (2003) Generisches Datenmanagement- und Kontrollsystem für gas-/flüssigkeitsdynamische Prüfstände. In: Virtuelle Instrumente in der Praxis (Begleitband zum Kongress VIP 2003), pp. 203-207. Hüthig, Heidelberg. 8. Anwenderkongress "Virtuelle Instrumente in der Praxis - VIP 2003", München, 12. - 13. 03. 2003. ISBN 3-7785-2908-0. Volltext nicht online.

Schmidt, V. and Sender, J. (1997) Thermischer Test keramischer Faserverbundwerkstoffe. DLR-Interner Bericht. 645-97/25. 117 S. Volltext nicht online.

Schmidt, V. and Sender, J. (1997) Thermischer Test keramischer Faserverbundwerkstoffe. Folgebericht: Untersuchungen nach Angebot 86456099. DLR-Interner Bericht. 645-97/29. 157 S. Volltext nicht online.

Schmidt, V. and Sender, J. and Oschwald, M. (2000) Flame Front Evolution and Liquid Phase Distribution During the Ignition Transient of a LOX/GH2-Combustor. In: 16th Annual Conference on Liquid Atomization and Spray Systems, X.4.1-X.4.6. ILASS-Europe 2000; 16th Annual Conference on Liquid Atomization and Spray Systems, Darmstadt, 11-13 September 2000. Volltext nicht online.

Schmidt, V. and Sender, J. and Oschwald, M. (2000) Simultaneous Observation of Liquid Phase Distribution and Flame Front Evolution during the Ignition transcient of a LOX/GH2-Combustor. In: 6th French-German Colloquium on Research in Liquid Rocket Propulsion. 6th French-German Colloquium on Research into Liquid Rocket Propulsion Phenomena, Heidelberg, 09. - 11. Oktober 2000. Volltext nicht online.

Schmidt, V. and Sender, J. and Oschwald, M. (2001) Simultaneous Observation of Liquid Phase Distribution and Flame Front Evolution during the Ignition Transcient of a LOX/GH2-Combustor. Journal of Visualization, 4 (4), pp. 365-372. Volltext nicht online.

Schmidt, V. and Sender J., and Haidn, O.J. (1999) Droplet Tracking Velocimetry in a Burning LOX/GH2-Spray. In: Proceedings of the Third International Workshop on PIV'99 - Santa Barbara, pp. 189-193. Third International Workshop on PIV'99, Santa Barbara (us), September 16-18, 1999. Volltext nicht online.

Schmidt, V. and Wepler, U. and Haidn, O. and Oschwald, M. (2004) Characterization of the Primary Ignition Process of a Coaxial GH2/LOX Spray. In: AIAA/ASME/SAE/ASEE Aero Space Sciences Meeting, pp. 1-10. 42nd AIAA/ASME/SAE/ASEE Aero Space Sciences Meeting, Reno, NV, January 5-8, 2004. Volltext nicht online.

Schmidt, Volker and Oschwald, Michael and Lacaze, G. (2009) Laser Ignition in a Micro Combustor. In: ProcessEng Engineering. pp. 97-131. ISBN 978-3-902655-05-9. Volltext nicht online.

Schmierer, Christian and Kobald, Mario and Fischer, Ulrich and Tomilin, Konstantin and Petrarolo, Anna and Hertel, Ferdinand (2019) Advancing Europe’s Hybrid Rocket Engine Technology with Paraffin and LOX. In: Proceedings of the 8th European Conference for Aeronautics and Space Sciences. 8th European Conference for Aeronautics and Space Sciences EUCASS, 2019-07-01 - 2019-07-04, Madrid, Spain. doi: 10.13009/EUCASS2019-682.

Schneider, G. (2004) Sprühstrahluntersuchungen an Showerhead-Injektoren der Firma EADS ST am Prüfstand M51. Project Report, DLR-Interner Bericht. 647-2004/10. 23 S. Volltext nicht online.

Scholl, Julian and Werling, Lukas and Freudenmann, Dominic and Schlechtriem, Stefan (2023) Activation Energy Determination of High-Test Peroxide Decomposition in Inconel 718 Crucibles. Aerospace Europe Conference 2023 – 10ᵀᴴ EUCASS – 9ᵀᴴ CEAS, 2023-07-09 - 2023-07-13, Lausanne, Schweiz. doi: 10.13009/EUCASS2023-553.

Schorpp, A. (1995) Entwicklung und Auslegung eines gekühlten optischen Zugangs für thermisch hoch belastete Brennkammern. DLR-Interner Bericht. 645-95/09 (Diplomarbeit FH Karlsruhe 95/07). Diploma. 74 S. Volltext nicht online.

Schröder, W. and Breede, F. and Danowski, C. and Grilli, M. and Hahn, M. and Hosters, N. and Klaus, M. and Kowollik, D. and Génin, C. and Schieffer, G. and Schlösser, J. and Tini, V. and Wallmerspreger, T. and Willems, S. (2011) SFB TRANSREGIO 40: SCHUBDÜSE. 60. Deutscher Luft- und Raumfahrtkongress , 2011-09-27 - 2011-09-29, Bremen. Volltext nicht online.

Schulz, U. and Fritscher, K. and Peters, M. and Greuel, Dirk and Haidn, Oskar (2005) Fabrication of TBC-armored rocket combustion chambers by EB-PVD methods and TLP assembling. Science and Technology of Advanced Materials, 6 (2), pp. 103-110. Volltext nicht online.

Schulz, Uwe and Fritscher, Klaus and Haidn, Oskar and Greuel, Dirk (2005) Fabrication and testing of EB-PVD thermal barrier coatings for Cu rocket combustion chambers. Material Science &Technology 05 Conference, 2005-09-25 - 2005-09-28, Pittsburgh, USA. (Unpublished) Volltext nicht online.

Schweitzer, C. and Schley, C.-A. (1997) H2/O2 Rocket Combustor Flow Field Modeling, Simulation and Analysis. In: 33rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Seattle, WA, July 7-9, 1997. Volltext nicht online.

Schäfer, K. (2002) Höhensimulationsprüfstand P4.1 für das VINCI Triebwerk. In: DGLR Jahrbuch 2002, Band II, pp. 899-907. DGLR. Deutscher Luft- und Raumfahrtkongress, Stuttgart, 23. - 26. September 2002. Volltext nicht online.

Schäfer, K. (1996) Hoehensimulation von Raketentriebwerken. In: Deutscher Luft- und Raumfahrt-Kongress, DGLR-Jahrestagung 1996, Dresden, 24.-27. September 1996, pp. 411-416. Volltext nicht online.

Schäfer, K. and Dommers, M. (2004) Alcohol LOX Steam Generator Test Experience. In: Space Propulsion 2004. 2nd International Conference on Green Propellants for Space Propulsion, Cagliari, Sardinia, Italy, 7-8 June 2004. Volltext nicht online.

Schäfer, K. and Haidn, O. (2003) The European Research and Test Center Lampoldshausen: Current Activities. Space Challenge in 21st Century. 100 Years after the Tsiolkovskiy Idea on Space Missions Using Reactive Motors, "SPACE 03", Moscow-Kaluga, September 15-19, 2003. Volltext nicht online.

Schäfer, K. and Krühsel, G. (2001) Advanced Green Propellant Steam Generator. In: Fourth International Conference on Green Propellants for Space Propulsion. 4th International Conference on Green Propulsion for Space Propulsion, Noordwijk, The Netherlands, 20-22 June 2001. Volltext nicht online.

Schäfer, K. and Zimmermann, H. (1999) Advanced Altitude Simulation for Future Upper Stage Engines and Satellites Systems. In: 12th European Aerospace Conference. 3rd European Conference on Space Transportation Systems: Meeting the Market Needs. 12th European Aerospace Conference. 3rd European Conference on Space Transportation Systems, Paris (France), Nov. 29-30, Dec. 1, 1999. Volltext nicht online.

Schäfer, K. and Zimmermann, H. (2002) Altitude Simulation Test Bench P4.1 for VINCI Upper Stage Engine. In: AAAF, 6th International Symposium for Space Transportation of the XXIst Century. AAAF, 6th International Symposium for Space Transportation of the XXIst Century, Paris, 14-17 May 2002. Volltext nicht online.

Schäfer, K. and Zimmermann, H. (2004) Simulation of Flight Conditions for Rocket Engine Qualification. In: Space Propulsion 2004. 2nd International Conference on Green Propellants for Space Propulsion, Cagliari, Sardinia, Italy, 7-8 June 2004. Volltext nicht online.

Schäfer, K. and Zimmermann, H. (2004) Simulation of Flight Conditions During Lift off for Rocket Engine Testing. In: AIAA/ASME/SAE/ASEE Joint Propulsion Conference, pp. 1-6. AIAA. 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Fort Lauderdale, FL, July 11-14, 2004. Volltext nicht online.

Schäfer, K. and Zimmermann, H. and Krühsel, G. (2003) Altitude Simulation Bench for VINCI Engine. In: 39th Joint Propulsion Conference and Exhibit. AIAA. 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Huntsville, AL, 20 - 23 July 2003. Volltext nicht online.

Schäfer, Klaus (2011) Kryo-Technikum Lampoldshausen. 13. Technologie-Transfer-Forum Lampoldshausen, 2011-11-24, Lampoldshausen, Deutschland. (Unpublished) Volltext nicht online.

Schäfer, Klaus (2011) Bürgerinformation zur Standortentwicklung Lampoldshausen. Bürger-Informationsveranstaltung im Rathaus Hardthausen, 2011-11-02, Hardthausen, Deutschland. (Unpublished)

Schäfer, Klaus (2012) Höhensimulation. Vorlesungsreihe Raumfahrtantriebe II, 2012-01-20, Aachen, Germany. (Unpublished) Volltext nicht online.

Schäfer, Klaus (2013) Herausforderungen an die Prüfstände für Raketenantriebe. DGLR-Raumfahrtkonferenz Missionen aus Baden-Württemberg, 2013-04-09, Stuttgart, Deutschland. (Unpublished) Volltext nicht online.

Schäffler, M. (1996) Experimentelle Untersuchung des Mischungsgebietes eines mit LN2/He betriebenen Koaxialinjektors. DLR-Interner Bericht. 645-96/11. 92 S. Volltext nicht online.

Schürmanns, K. (1999) Experimentelle Untersuchung zur Vermischung von Wasserstoff in einer Unterschall-Staubrennkammer. Dissertation, Rheinisch-Westfälische Technische Hochschule Aachen, Fakultät für Maschinenwesen. Volltext nicht online.

Schürmanns, K. and Ciezki, H. and Feinauer, A. and Schneider, A. (1998) Experimentelle Bestimmung der Massenstrom-Geschwindigkeits- und Totaldruckverteilungen in den AUDI-Luftansaugungen der Baustufen 1 und 2. DLR-Interner Bericht. 645-98/17. 25 S. Volltext nicht online.

Schürmanns, Rainer (2009) Das Raumfahrtzentrum Guyana (CSG), Europas Weltraumbahnhof. In: Tagungsband. Deutscher Luft- und Raumfahrtkongress 2009, 2009-09-08 - 2009-09-10, Aachen, Deutschland. ISBN 978-3-932182-63-4. ISSN 1868-8756. Volltext nicht online.

Schürmanns, Rainer (2010) Eine Ariane Startkampagne in Kourou. Deutscher Luft- und Raumfahrtkongress 2010, 2010-08-31 - 2010-09-02, Hamburg, Deutschland. ISBN 978-3-932182-68-5. ISSN 1868-8764. Volltext nicht online.

Schürmanns, Rainer (2011) Aspekte der Instandhaltung von Raketenprüfständen. 1. Mosbacher Industrieforum, 2011-05-24, Mosbach, Deutschland. Volltext nicht online.

Schürmanns, Rainer (2011) Risikobeherrschung einer Ariane Kampagne. PM-Days im DLR, 2011-06-08 - 2011-06-09, Köln, Deutschland. Volltext nicht online.

Schürmanns, Rainer (2011) Launcher components' integration with payloads. In: Proceedings. Deutscher Luft- und Raumfahrtkongress 2011, 2011-09-27 - 2011-09-29, Bremen, Deutschland. Volltext nicht online.

Schäfer, K. and Krühsel, G. and Schmidt, V. and Haidn, O. and Oschwald, M. and Suslov, D. (2007) Methane / Oxygen Test Facilities in Lampoldshausen. 2nd European Conference on Aerospace Sciences EUCASS, 2007, Brussels (B). Volltext nicht online.

Schäfer, Klaus and Zimmermann, Herbert and Kronmüller, Harald and Böhm, Christian (2005) P4.1 Test Facility for Altitude Simulation of VINCI Engine, Bench Development. In: 2005 Moscow EUCASS. EUCASS 2005, 2005-07-04 - 2005-07-07, Moscow. Volltext nicht online.

Schäfer, Klaus (2005) Simulation Of Environmental Flight Conditions By Advanced Altitude Simulation. 2005 6th International Symposium on Launcher Technologies, 2005-11-08 - 2005-11-11, Munich, Germany.

Schäfer, Klaus and Böhm, Christian and Kronmüller, Harald and Stark, Ralf and Zimmermann, Herbert (2005) P6.2 Cold Gas Test Facility For Simulation of Flight Conditions - Current Activities. In: 2005 European Conference for Aerospace Sciences, pp. 1-7. EUCASS 2005, 2005-07-04 - 2005-07-07, Moscow, Russia.

Schäfer, Klaus and Böhm, Christian and Kronmüller, Harald and Zimmermann, Herbert (2005) Development of P4.1 Altitude Simulation for VINCI Engine. In: 2005 Deutscher Luft- und Raumfahrtkongress, pp. 1-10. DGLR 2005, 2005-09-26 - 2005-09-29, Friedrichshafen.

Schäfer, Klaus and Frank, Anja (2016) European Test Center DLR Lampoldshausen, Shaping The Future. In: Space Propusion Conference 2016. Space Propulsion 2016, 2016-05-02 - 2016-05-06, Rom, Italien. Volltext nicht online.

Schäfer, Klaus and Krühsel, Gerhard (2005) Test Platforms of LOX/Ethanol Rocket Steam Generators at DLR Lampoldshausen. In: 2005 European Conference for Aerospace Sciences, pp. 1-8. EUCASS 2005, 2005-07-04 - 2005-07-07, Moscow, Russia.

Schäfer, Klaus and Zimmermann, Herbert and Pauly, Clement (2008) Development and Operational Conditions of VINCI Altitude Simulation Test Bench P4.1. In: 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 2008-07-21 - 2008-07-23, Hartford, CT (USA).

Searby, G. and Haidn, O. and Habiballah, M. and Boronine, E. and Thomas, J. and Durand, P. (2000) Present Status of the High Frequency Combustion Instability Program. In: 6th French-German Colloquium on Research in Liquid Rocket Propulsion. 6th German-French Colloquium on Research into Liquid Rocket Propulsion Phenomena, Heidelberg, 09. - 11. Oktober 2000. Volltext nicht online.

Searby, G. and Haidn, O. and Habiballah, M. and Pauchet, J. (1999) High Frequency Combustion Instability Program. In: Fifth French-German Colloquium Research on Liquid Rocket Propulsion. Fifth French-German Colloquium Research on Liquid Rocket Propulsion. Volltext nicht online.

Selzer, Markus and Peichl, Jonas Stefan and Hoffmann, Ivens Daniel and Suslov, Dmitry (2023) Outflow measurements on porous injector elements. In: Aerospace Europe Conference 2023 – 10ᵀᴴ EUCASS – 9ᵀᴴ CEAS. Aerospace Europe Conference 2023 – 10ᵀᴴ EUCASS – 9ᵀᴴ CEAS, 2023-07-09 - 2023-07-13, Lausanne, Schweiz. doi: 10.13009/EUCASS2023-566. Volltext nicht online.

Sender, J. and Ciezki, H. (1996) Velocities of Reacting Boron Particles in a Solid Fuel lRamjet Combustion Chamber. Intern. Seminar on High Energy Materials (HEM), Pune, India, Nov. 19-21, 1996. Volltext nicht online.

Sender, J. and Ciezki, H. (1996) Geschwindigkeitsmessungen an reagierenden Borpartikeln in einer Feststoff-Brennkammer. Vortrag bei: Lasermethoden in der Stroemungsmesstechnik, (Galatagung), Berlin, 11.-13. Sept. 1996. Volltext nicht online.

Sender, J. and Ciezki, H.K (1997) Velocities of Reacting Boron-Particles within a Solid Fuel Ramjet Combustion Chamber. Internationales Seminar on High Energy Materials (HE11), Pune, India, November 19-21, 1996. Volltext nicht online.

Sender, J. and Schmidt, V. and Bonnet, J. and Oschwald, M. and Haidn, O. (1997) Geschwindigkeitsfeld und Flammenemission eines brennenden LOX/GH2-Sprays. In: Spray '97. Spray '97: 3rd Workshop über Sprays, Erfassung von Sprühvorgängen und Techniken der Fluidzerstäubung, Lampoldshausen, 22. - 23. Oktober 1997. Volltext nicht online.

Sender, J. and Schmidt, V. and Oschwald, M. and Lecourt, R.(1) (1997) Movement of LOX Droplets in a Burning LOX/GH2 Spray at Pressure up to 1.2 MPa. In: 3rd French-German Colloquium on Research on Liquid Rocket Propulsion, Marseille, France, June 5-6, 1997. Volltext nicht online.

Serbest, E. and Fritscher, K. and Haidn, O. and Hald, H. and Korger, G. and Winkelmann, P. (2000) Advanced Materials for Thrust Chamber Technologies. In: Fourth International Symposium on Liquid Space Propulsion - Scientific Progress in the Service of Space Access at the Beginning of the Third Millennium -. 4th International Symosium on Space Propulsion, Heilbronn, March 13-15, 2000. Volltext nicht online.

Serbest, E. and Haidn, O. and Greuel, D. and Hald, H. and Korger, G. (2001) Effusion Cooling of Throat Region in Rocket Engines Applying Fibre Reinforced Ceramics. In: 37th Joint Propulsion Conference and Exhibit. 37th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Salt Lake City, Utah, 8-11 July 2001. Volltext nicht online.

Serbest, E. and Haidn, O. and Hald, H. and Korger, G. and Winkelmann, P. and Fritscher, K. (1999) Advanced Technologies and Materials for Future Liquid Rocket Engines. In: 12th European Aerospace Conference. 3rd European Conference on Space Transportation Systems: Meeting the Market Needs. 12th European Aerospace Conference. 3rd European Conference on Space Transportation Systems, Paris (France), Nov. 29-30, Dec. 1, 1999. Volltext nicht online.

Serbest, E. and Haidn, O.J. and Hald, H. and Korger, G. and Winkelmann, P. (1999) Einsatz von poröser Faserkeramik für Effusionskühlung in Raketenbrennkammern. In: DGLR Jahrbuch 1999, pp. 949-958. DGLR-Jahrestagung, Berlin (de), 27. bis 30. September 1999. Volltext nicht online.

Serbest, E. and Haidn, O.J. and Hald, H. and Korger, G. and Winkelmann, P. (1999) Effusion Cooling in Rocket Combustors Applying Fiber Reinforced Ceramics. In: 35th Joint Propulsion Conference. 35th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Los Angeles, CA, June 20-24, 1999. Volltext nicht online.

Simonsen, J.P. (1997) Investigation of the Shear Layer Development in the Planar Step Combustor of Test Facility M11.2. DLR-Interner Bericht. 645-97/27. 62 S. Volltext nicht online.

Simonsen, J.P. (1998) Investigation of the Shear Layer Development in the Planar Step Combustor of Test Facility M11.2. DLR-Interner Bericht. 645-98/07. 64 S. Volltext nicht online.

Sippel, M. (2000) Etudes des Trajectoires et Performances du Petit Lanceur Px/Hy. Project Report. DLA/SDT/SP/660/00. Centre National D'Etudes Spatiales (CNES). 23 S. Volltext nicht online.

Sippel, M. (2000) Etudes des Trajectoires et Performances d'ARIANE 2010 avec EAP Amélioré. Project Report. DLA/SDT/SP/673/00. Centre National d'Etudes Spatiales (CNES). 16 S. Volltext nicht online.

Sippel, M. (2000) Comparaison des Performances Calculees par les Logiciels ALTOS et OPTAX. Project Report. CNES DLA7SDT/SP/698/2000. Centre National D'Etudes Spatiales (CNES). 13 S. Volltext nicht online.

Sippel, M. (2000) Abaques des Masses Iajecties AR5 2010 en fonction de l'ESC. Project Report. DLA/SDT/SP/743/2000. Centre National d'Etudes Spatiales (CNES). 4 S. Volltext nicht online.

Sippel, M. (2001) Parametrische Untersuchung des Antriebskonzeptes für ein supersonisches Trägerflugzeug als Erststufe eines Raumtransportsystems. DLR-Forschungsbericht. 2001-08. Dissertation. 189 S. Volltext nicht online.

Sippel, M. (2004) Concurrent Launcher Engineering at DLR. In: Concurrent Engineering Workshop, pp. 1-8. Concurrent Engineering Workshop, ESTEC, Noordwijk, 30.09. - 01.10. 2004. Volltext nicht online.

Sippel, M. and Atanassov, U. and Kauffmann, J. and Klevanski, J. and Schmid, V. (2001) Reusable Hydro-Carbon Booster Stages as a Replacement for Large Solid Rocket Motors. In: Fourth International Conference on Green Propellants for Space Propulsion. 4th International Conference on Green Propulsion for Space Propulsion, Noordwijk, The Netherlands. Volltext nicht online.

Sippel, M. and Atanassov, U. and Klevanski, I. and Schmid, V. (2001) First Stage Design Variations of Partially Reusable Launch Vehicles. In: International Space Flanes & Hypersonic Systems & Technologies Conference. AIAA. 10th AIAA-NASDA-NAL-ISAS International Space Planes Conference, Kyoto, Japan, April 2001. Volltext nicht online.

Sippel, M. and Atanassov, U. and Klevanski, J. and Schmid, V. (2002) First Stage Design Variations of Partially Reusable Launch Vehicles. Journal of Spacecraft and Rockets, 39 (4), pp. 571-579. Volltext nicht online.

Sippel, M. and Burkhardt, H. and Klevanski, J. (2003) Options for High Performance, Low Cost Experimental Flight Vehicles. In: International Symposium Atmospheric Reentry, Vehicles and Systems, pp. 1-11. 3rd International Symposium Atmospheric Reentry, Vehicles and Systems, Arcachon, 24. - 27. March 2003. Volltext nicht online.

Sippel, M. and Burkhardt, H. and Klevanski, J. and Herbertz, A. (2004) Technical Assessment of the French RLV Concepts EVEREST and RFS. DLR-Interner Bericht. 647-2004/02. 72 S. Volltext nicht online.

Sippel, M. and Burkhardt, H. and Klevanski, J. and Herbertz, A. (2004) ASSC-2 (Liquid Fly Back Booster with Ariane 5) Liquid Fly Back Booster Stage Requirements. DLR-Interner Bericht. 647-2004/06. 26 S. Volltext nicht online.

Sippel, M. and Herbertz, A. (2002) High Thrust Bleed Rocket Engines for a Fly-Back Booster Application. In: International Symposium on Propulsion for Space Transportation of the XXIst century, pp. 1-10. 6th International Symposium on Propulsion for Space Transportation of the XXI Century, Palais des Congress, Versailles, France, 14 - 17 May 2002. Volltext nicht online.

Sippel, M. and Herbertz, A. and Haeseler, D. and Götz, A. (2002) Feasibility of High Thrust Bleed Cycle Engines for Reusable Booster Applications. In: 4th International Conference on Launcher Technology "Space Launcher Liquid Propulsion". 4th International Conference on Launcher Technology "Space Launcher Liquid Propulsion", Liege, 3 - 6 December 2002. Volltext nicht online.

Sippel, M. and Kauffmann, J. and Schmid, V. (2000) Studie zu Organisationsstruktur und Arbeitsweise der US-Trägerraketen-Hersteller Lookheed-Martin und Boeing bei der Entwicklung/Produktion und Vermarktung neuer Fahrzeugsysteme. Project Report, DLR-Interner Bericht. 645-2000/28. 14 S. Volltext nicht online.

Sippel, M. and Kauffmann, Jens (2003) Propulsion 2000 Phase 2 Solar Thermal Propulsion for Upper Stages. Project Report, DLR-Interner Bericht. 647-2003/13. 25 S. Volltext nicht online.

Sippel, M. and Klevanski, J. (2003) Progress in Simulating the Advanced In-Air-Capturing Method. In: 5th International Conference on Launcher Technology. Space Launchers: Missions, Control and Avionics. 5th International Conference on Launcher Technology, Madrid, 25. - 27. November 2003. Volltext nicht online.

Sippel, M. and Klevanski, J. (2004) Preliminary Definition of an Aerodynamic Configuration for a Reusable Booster Stage within Tight Geometric Constraints. In: 5th European Symposium on Aerothermodynamics for Space, pp. 1-6. 5th European Symposium on Aerothermodynamics for Space Vehicles, Köln, 08.-11. Nov. 2004. Volltext nicht online.

Sippel, M. and Klevanski, J. and Atanassov, U. (2004) Search for Technically Viable Options to Improve RLV by Variable Wings. In: 55th International Astronautical Congress, pp. 1-12. IAF. IAF, Vancouver, 4.-10. Oct. 2004. Volltext nicht online.

Sippel, M. and Klevanski, J. and Atanassov, U. and Schmid, V. (2001) Documentation of the DLR Design Activities Concerning the Liquid Fly Back Booster Concepts ASSC-2 V. Project Report, DLR-Interner Bericht. 645-2001/09. 94 S. Volltext nicht online.

Sippel, M. and Klevanski, J. and Burkhardt, H. (2002) Progress in the Design of a Reusable Launch Vehicle Stage. In: 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. AIAA. 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Indianapolis, IN, 7 - 10 July 2002. Volltext nicht online.

Sippel, M. and Klevanski, J. and Kauffmann, J. (2001) Innovative Method for Return to the Launch Site of Reusable Winged Stages. In: International Astronautical Congress. 52nd International Astronautical Congress, Toulouse, 1.-5. Oct. 2001. Volltext nicht online.

Sippel, M. and Koschel, W. (2000) Parametrical Analysis of Near-Term Air-Breathing Engine Concepts for First Stage Space Plane Acceleration Missions. In: 36th Joint Propulsion Conference and Exhibit. 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Huntsville, AL, July 17-19, 2000. Volltext nicht online.

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This list was generated on Fri Apr 11 20:20:18 2025 CEST.