Technology demonstration advanced storable propellaet turbopump engine

34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 1998, Pages 1-12

  Langel, G ^a   Obermaier, G ^a   Taubenberger, G ^a   Pierro, R ^a  

^a AIRBUS GROUP INNOVATIONS   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

COMBUSTION CHAMBERS; DEMONSTRATIONS; FLAMMABILITY TESTING; MANUFACTURE; PROPULSION; SEA LEVEL; TURBINE PUMPS;

COMBUSTION STABILITY; ENGINE DEVELOPMENT; FEASIBILITY TESTING; FUNCTIONAL MODIFICATION; MANUFACTURING PROCESS; OPERATIONAL CONDITIONS; REGENERATIVELY COOLED; TECHNOLOGY DEMONSTRATION PROGRAMS;

ENGINES;

EID: 84963811902     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (8)

1. G. Schmidt, G. Langel, H. Zewen Development Status of the Ariane 5 Upper-Stage Aestm Engme,AIAA-93-2131, 29th Joint Propulsion Conference, Monterey, June 1993
2. G. Langel, E. Laudien, R. Pongratz Combustion Stability Characteristics of the Ariane 5 L7 Engine, IAF-91-250, Montreal, October 1991
3. D. Feyhl, K. Eckert, H. Zewen Aestus Engine Experience, 5th International Symposium,Propulsion in Space, Paris, May 1996
4. K. Butler, G. Langel Storable Upper Stage Engine for Global Applications AIAA-97-3347, 33rd Joint Propulsion Conference, Seattle, July 1997
5. G. Obermaier, G. Taubenberger, D. Feyhl Coaxial Injector Development for Starable Propellant Upper Stage Turbopump Engines AIAA-97-3095, 33rd Joint Propulsion Conference, Seattle, July 1997
6. G. Schmidt, G. Langel, H. Zewen Coaxial Injection Technology for Hypergolic Propellants.Pmceedmgs of the 2nd European Aerospace Conference on Progress in Space Transportation, Bonn-Bad Godesberg, FRG, 1989
7. O. Knab, D. Preclik, D. Estublier Flow Field Prediction within Liquid Film Cooled Combustion Chambers of Storable Bi-Propellant Rocket Engines, AIAA-98-3370, 34rd Joint Propulsion Conference, Cleveland, Ohio, July 1998
8. Liquid Rocket Engine Combustion Stabilization Devices, NASA Space Vehicle Design Criteria, NASA-SP-8113