Development and testing of C/SiC components for liquid rocket propulsion applications

35th Joint Propulsion Conference and Exhibit

Volumn , Issue , 1999, Pages

  Beyer, S ^a   Strobel, F ^a   Knabe, H ^a  

^a DAIMLER AG   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

COMBUSTION CHAMBERS; COST EFFECTIVENESS; CRYOGENICS; ENGINES; EXPANSION; FIBER REINFORCED PLASTICS; GLASS CERAMICS; HIGH TEMPERATURE EFFECTS; HYPERSONIC VEHICLES; LOW TEMPERATURE PRODUCTION; NOZZLES; PROPELLANTS; REUSABILITY; ROCKETS; SPACECRAFT PROPULSION;

COST-EFFECTIVE PRODUCTION; DEVELOPMENT AND TESTING; HIGH TEMPERATURE COMPONENTS; LIQUID ROCKET PROPULSION; PRODUCTION TECHNOLOGY; PROPULSION SYSTEM COMPONENTS; SPACE PROPULSION SYSTEM; THERMOCHEMICAL PROPERTIES;

TOXIC MATERIALS;

EID: 84963864749     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1999-2896     Document Type: Conference Paper

References (2)

1. W. Schafer, S. Beyer, U. Trabandt, “Ceramic fiber-reinforced composites for hot space structures”, DGLR Symposium 1998, Bremen, Germany.
2. W. Schafer, H. Knabe, D. Scheulen, W. D. Vogel “Hot Aerospace Structures from Fiber Reinforced Ceramics”, 17th Conference Aerospace Material Engineering, Paris, 1997.