Technology developments for cryogenic rocket engines

36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2000, Pages

  Immich, H ^a   Kretschmer, J ^a   Preclik, D ^a  

^a AIRBUS DEFENCE AND SPACE   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

C (PROGRAMMING LANGUAGE); CERAMIC COATINGS; CERAMIC MATERIALS; CHROMIUM COMPOUNDS; CRYOGENICS; ENGINES; FIRES; METALLOGRAPHY; NICKEL COMPOUNDS; NOZZLES; PIPE LININGS; PROPULSION; ROCKETS; TRANSPIRATION; ZIRCONIA;

CERAMIC NOZZLES; CHAMBER DESIGN; COATING TECHNOLOGIES; METALLOGRAPHIC ANALYSIS; TECHNOLOGY DEVELOPMENT; TECHNOLOGY PROGRAMMES; THRUST CHAMBER; TRANSPIRATION COOLING;

THERMAL BARRIER COATINGS;

EID: 85085775234     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2000-3780     Document Type: Conference Paper

References (11)

1. Nicolay, R., Mattstedt, T., Thelemann, D., "Status of Cryogenic Thrust Chamber Developments for the Ariane 5 Launcher", Paper AIAA-2000-3167, 36th Joint Propulsion Conference, Huntsville, AL, 2000.
2. Mattstedt, T.B., Haidinger, F.A., Hensel, C., "Development of the Thrust Chamber for the New Cryogenic Upper Stage Engine of Ariane 5", Paper AIAA-99-2601, 35th Joint Propulsion Conference, Los Angeles, CA, 1999.
3. Immich, H., Mayer, W., "Cryogenic Liquid Rocket Engine Technology Developments within the German National Technology Programme", Paper AIAA-97-2822, 33rd Joint Propulsion Conference, Seattle, WA, 1997.
4. Mayer, W., 'The German National Technology Program on Cryogenic Rocket Engines at DLR", Paper AIAA-2000-3219, 36th Joint Propulsion Conference, Huntsville, AL, 2000.
5. Immich, H., Frohlich, T., Kretschmer, J., 'Technology Developments for Expander Cycle Engine Thrust Chambers", Paper AIAA-99-2889, 35th Joint Propulsion Conference, Los Angeles, CA, 1999.
6. Haeseler D. et al., "Experimental Investigation of Transpiration-Cooled Hydrogen-Oxygen Subscale Chambers", Paper AIAA-98-3364, 34th Joint Propulsion Conference, Cleveland, OH, 1998.
7. Preclik, D., Wiedmann, D., Oechslein, W. and Kretschmer, J., "Cryogenic Rocket Calorimeter Chamber Experiments and Heat Transfer Simulations", Paper AIAA-98-3440, 34th Joint Propulsion Conference, Cleveland, OH, 1998.
8. Gorgen, J., Knab, O. and Wennerberg, D., "Impact of Intentional and Unintentional Combustion Chamber Porosity on Rocket Engine Characteristics", Paper presented at the Fourth International Symposium on Liquid Space Propulsion, DLR-Lampoldshausen, Germany, March 12-15, 2000.
9. Beyer, S., Knabe, H., Strobel, F., "Development and Testing of C/SiC Components for Liquid Rocket Propulsion", Paper AIAA-99-2896, 35th Joint Propulsion Conference, Los Angeles, CA, 1999.
10. Frey, M., and Hagemann, G., "Restricted Shock Separation in Rocket Nozzles," Journal of Propulsion and Power, Vol. 16, No. 3, May- June 2000.
11. Frey, M., and Hagemann, G., "Flow Separation and Side-Loads in Rocket Nozzles," AIAA Paper 99-2815, 1999.