Cryogenic liquid rocket engine technology developments within the german national technology programme

33rd Joint Propulsion Conference and Exhibit

Volumn , Issue , 1997, Pages

  Immich, Hans ^a   Mayer, Wolfgang ^b  

^a AIRBUS GROUP INNOVATIONS   (Germany)

^b GERMAN AEROSPACE CENTER DLR   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

CARBON; CARBON FIBERS; COMBUSTION CHAMBERS; CRYOGENICS; ENGINES; FIBER REINFORCED MATERIALS; FIBER REINFORCED PLASTICS; HEAT TRANSFER; LAUNCH VEHICLES; LIQUIDS; PROPULSION; REUSABILITY; ROCKET ENGINES; ROCKETS; THERMAL BARRIER COATINGS;

CARBON FIBRE REINFORCED COMPOSITE MATERIALS; LIQUID ROCKET ENGINES; LIQUID ROCKET PROPULSION; REGENERATIVELY COOLED; REUSABLE LAUNCH VEHICLES; TECHNOLOGY DEVELOPMENT; TECHNOLOGY PROGRAMMES; VEHICLE PROPULSION SYSTEMS;

BOOSTERS (ROCKET);

EID: 84962909482     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (20)

1. Popp, M., Pekkari, L.-O., 'Cryogenic Engine Thrust Chamber Technologies', Paper 4.3, 5th AAAF Transportation, Paris, France, 1996
2. Kuczera, H., Sacher, P.W., Dujarric, Ch., 'FESTJP System Study-An Overview', Paper presented at the 7th International Space Planes and Hypersonic Systems and Technologies Conference, November 18-22, 1996, Norfolk, VA/USA
3. Zinner, W. et al., 'Development of Advanced Technologies for Future Cryogenic Thrust Chamber Applications', Paper AIAA-97-3312, 33rd Joint Propulsion Conference, Seattle, WA, 1997.
4. Popp, M., Schmidt, G., 'Rocket Engine Combustion Chamber Design Concepts for Enhanced Life', AIAA 96-3303, 32nd Joint Propulsion Conference; July 1-3, 1996 / Lake Buena Vista, FL
5. Sassnick, H.-D., Krulle, G., 'Numerical Simulation of Transients in Feed Systems of Cryogenic Rocket Engines', AIAA 95-2967, San Diego, CA, 1995
6. Neuner, F., Preclik, D., Zinner, W., Dittmann, A., 'Weiterentwicklung von Vorhersagemethoden zur Beschreibung des Warmeiibergangs in Raketenbrennkammern', DGLR Jahrestagung 1996, Dresden, 24.-27.9. 1996
7. Schley, C.-A., Preclik, D., 'Combustion Chamber Code Activities in Germany', 2nd French-German Colloquium on Research in Liquid Rocket Propulsion, Aachen, May 30-31, 1996
8. Frohlich, A., Immich, H., Le Bail, F., Popp, M., Three Dimensional Flow Analysis in a Rocket Engine Coolant Channel of High Depth/Width Ratio', AIAA 91-2183, 27th Joint Propulsion Conference, Sacramento, CA, 1991
9. Le Bail, F., Popp, M., 'Numerical Analysis of High Aspect Ratio Cooling Paasage Flow and Heat Transfer', AIAA 93-1829, 29th Joint Propulsion Conference, Monterey, CA, 1993
10. Froehlke, K., Haberzettl, A., Haidn, O., Heinrich, S., Sion, M., Vuillermoz, P., 'First hot fire test campaign at the French/german research facility P81, AIAA 97-2929, 33rd Joint Propulsion Conference, Seattle, WA, 1997.
11. Schley, C.-A., Hagemann, G., Golovitchev, V., 'Comparison of H2/O2 Rocket Model Engine Reference Simulations', AIAA 95-2429, San Diego, 1995
12. Schweitzer, C., Schley, C.-A, 'H2/O2 Rocket Combustor Row Field Modelling, Simulation and Analysis', AIAA 97-3300, 33rd Joint Propulsion Conference, Seattle, WA, 1997.
13. Mayer, W., Schik, A., Schweitzer, C., Schaffler, M., 'Injection and Mixing Processes in High Pressure LOX/GH, Rocket Combustor', AIAA 96-2620, 32th AIAA Joint Propulsion Conference, Lake Buena Vista, FL, 1996
14. Mayer, W., Tamura, H., 'Flow Visualization of Supercritical Propellant Injection in a Firing LOX/GH2 Rocket Engine', AIAA 95-2433, Journal of Propulsion and Power, Vol. 12, No.6,pp 1137-1147, 1996
15. Froehlke, K., Haidn, O., Kuhl, D. 'Requirements for H2/O2 steam generators', 3rd Int. Conf. on Energy Systems and Conversions, Kazan, Russia, to be published, 1997
16. Oschwald, M., Lecourt, R., Brummund, U., Cessou, A., Haidn, O., 'Optical Diagnostics of Atomization and Combustion for Cryogenic Liquid Rocket Propulsion', 4th Internationl Symposium on Special Topics in Chemical Propulsion, Stockholm, Sweden, 1996
17. Quentmeyer, R.J., 'Rocket Combustion Chamber Life-Enhancing Design Concepts', AIAA-90-2116, 26th Joint Propulsion Conference, Orlando, FL, 1990.
18. Fisher, S.C.; Popp M.; Quentmeyer R.J.; 'Liquid Rocket Combustion Devices-Aspects of Modelling, Analysis, and Design: Thrust Chamber Cooling and Heat Transfer', Proceedings of the Second International Symposium on Liquid Rocket Propulsion; edited by M. Habiballah, M. Popp, and V. Yang, Mai 1995
19. Wadel, M. F. and Meyer, M.L, 'Validation of High Aspect Ratio Cooling in a 89kN (20,000 Ibf) Thrust Combustion Chamber' AIAA 96-2584, 32nd Joint Propulsion Conference; July 1-3, 1996 / Lake Buena Vista, FL
20. Hald, H., 'CMC Materials: From Plasma Channel Test to Real Capsule Reentry', High Temperature Chemical Processes 3, pp. 153-165, 1994.