Thrust chamber technology developments for future launch vehicle liquid rocket engines

37th Joint Propulsion Conference and Exhibit

Volumn , Issue , 2001, Pages

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

^a AIRBUS DEFENCE AND SPACE   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

CERAMIC MATRIX COMPOSITES; COMBUSTION CHAMBERS; ENGINES; LIQUEFIED GASES; NOZZLES; PROPULSION; ROCKETS; THERMAL BARRIER COATINGS; WELL TESTING;

CHAMBER EXPERIMENTS; ENABLING TECHNOLOGIES; HEAT TRANSFER MEASUREMENTS; LIQUID ROCKET ENGINES; PROPELLANT INJECTION; SPACE INFRASTRUCTURES; STAGED COMBUSTION CYCLE ENGINE; TECHNOLOGY DEVELOPMENT;

HEAT TRANSFER PERFORMANCE;

EID: 85088722229     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-3544     Document Type: Conference Paper

References (10)

1. Immich, H., Kretschmer, J., D. Preclik, Technology Developments for Cryogenic Rocket Engines', Paper AIAA-2000-3780, 36th Joint Propulsion Conference, Huntsville, AL, 2000.
2. 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.
3. 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.
4. Alting, J., Grauer, F., Hagemann, G.,Kretschmer, J., 'Hot-Firing of an Advanced 40 kN Thrust Chamber', Paper AIAA-2001-3260, 37th Joint Propulsion Conference, Salt Lake City, UT, 2001.
5. Mattstedt, T. et al., 'Full-Scale Development of Advanced Expander Cycle Thrust Chambers', Paper AIAA-2001-3999, 37th Joint Propulsion Conference, Salt Lake City, UT, 2001.
6. 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.
7. Wennerberg, D., Knab, O., 'Effective Calculation of Multi-phase Flow Fields in Liquid Rocket Thrust Chambers', Paper AIAA- 2001-4878, 37th Joint Propulsion Conference, Salt Lake City, UT, 2001.
8. 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.
9. Hagemann, G., Terhardt, M., Haeseler, D., Frey, M., 'Experimental and Analytical Design Verification of the Dual-Bell Concept', Paper AIAA-2000-3778, 36th Joint Propulsion Conference, Huntsville, AL, 2000.
10. Hagemann, G., Immich, H., Dumnov, G., 'Critical Assessment of the Linear Plug Nozzle Concept', Paper AIAA-2001-4865, 37th Joint Propulsion Conference, Salt Lake City, UT,2001.