Development of the thrust chamber for the new cryogenic upper stage engine of AR1ANE5

35th Joint Propulsion Conference and Exhibit

Volumn , Issue , 1999, Pages

  Mattstedt, T B ^a   Haidinger, F A ^a   Hensel, C ^a  

^a DAIMLER AG   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

CRYOGENICS; ECONOMIC AND SOCIAL EFFECTS; NOZZLE DESIGN; NOZZLES; PROPULSION;

BEST CHOICE; CRYOGENIC ENGINES; ECONOMIC ADVANTAGES; NOZZLE EXTENSION; PRESENT STATUS; THRUST CHAMBER; TRADE-OFF STUDY; UPPER STAGES;

ENGINES;

EID: 84963865490     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (6)

1. H. Immich, G. Langel, M. Popp, “Rocket Engine Thrust Chamber Developments for Future Launch Vehicles”, IAF-98-S.3.03, 49th Interna-tional Astronautical Congress, Sept. 28 -Oct 2, 1998, Melbourne, Australia.
2. G. Langel, M. Popp, G. Schmidt, G. Obermaier, “DASA Propulsion Activities for Future Ariane5 Upper Stage Improvements”, DGLR-JT97-110, Deutscher Luft-und Raumfahrtkongress 1997, DGLR Jahrestagung, Oct. 14 -17, 1997, Munich, Germany.
3. G. Schmidt, M. Popp, T. Frohlich, “Design Stud-ies for a 10 Ton Class High Performance Ex-pander Cycle Engine”, AIAA 98-3673, 34th Joint Propulsion Conference, July 12 -15, 1998, Cleveland, OH.
4. G. Langel, G. Obermaier, G. Taubenberger, R. Pierro, Technology Demonstration for Advanced Storable Propellant Turbopump Engines”, AIAA 98-3677, 34th Joint Propulsion Conference, July 12-15,1998, Cleveland, OH.
5. F. Jean, P. Girard, T. Mattstedt, J.M. Ruault, “A New Cryogenic Upper Stage Engine”, IAF-98-S1.05, 49th International Astronautical Congress, Sept. 28 -Oct 2,1998, Melbourne, Australia.
6. C. Hensel, T. Mattstedt, W. Oechslein, M. de Wilde, “Ignition System Concept for the New Cryogenic Upper Stage Engine of Ariane 5”, AIAA 99-2474, 35th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Los Angeles, CA, June 20-23, 1999