Coaxial injector development for storable propellent upper stage turbopump engines

33rd Joint Propulsion Conference and Exhibit

Volumn , Issue , 1997, Pages

  Obermaier, G ^a   Taubenberger, G ^a   Feyhl, D ^a  

^a AIRBUS GROUP INNOVATIONS   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

FLAMMABILITY TESTING; LAUNCH VEHICLES; MANUFACTURE; PROPELLANTS; PROPULSION; TURBINE PUMPS;

CO-AXIAL INJECTORS; COMBUSTION STABILITY; DEMONSTRATION TESTS; DEVELOPMENT HISTORY; ENGINE DEVELOPMENT; EXCELLENT MANUFACTURING; MANUFACTURING PROCESS; OPERATIONAL CONDITIONS;

ENGINES;

EID: 34249330029     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (7)

1. 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
2. G. Schmidt, G. Langel, H. Zewen, Development Status of the Ariane 5 Upper-Stage Aestus Engine, AIAA-93-2131, 29th Joint Propulsion Conference, Monterey, June 1993
3. G. Langel, E. Laudien, R. Pongratz, Combustion Stability Characteristics of the Ariane 5 L7 Engine, IAF-91-250, Montreal, October 1991
4. D. Feyhl, K. Eckert, H. Zewen, Aestus Engine Experience, 5th International Symposium,Propulsion in Space, Paris, May 1996
5. K. Butler, G. Langel, Storable Upper Stage Engine for Global Applications AIAA-97-3347, 33rd Joint Propulsion Conference, Seattle, July 1997
6. S. Gordon, B.J. McBride, Computer Program for Calculation of Complex Chemical Equilibrium Compostions and Rocket Performance, CET89, NASA SP-273
7. Liquid Rocket Engine Combustion Stabilization Devices, NASA Space Vehicle Design Criteria, NASA-SP-8113