Development of a new cost-effective ceramic composite for re-entry heat shield applications

Acta Astronautica

Volumn 42, Issue 9, 1998, Pages 533-540

  Muhlratzer A ^a   Handrick, K ^a   Pfeiffer, H ^a  

^a MAN Technologie GmbH   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

CERAMIC MATRIX COMPOSITES; COMPRESSIVE STRENGTH; COST EFFECTIVENESS; HEAT SHIELDING; IMPREGNATION; LAMINATED COMPOSITES; PYROLYSIS; REENTRY; REINFORCEMENT; SHEAR STRENGTH; TENSILE STRENGTH; THERMAL GRADIENTS;

ADVANCED CREW TRANSFER VEHICLES; REENTRY CAPSULES;

SPACECRAFT;

EID: 0032068942     PISSN: 00945765     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0094-5765(97)00220-8     Document Type: Article

References (7)

1. Sygulla, D., Mühlratzer, A. and Agatonovic, P., Integrated approach in modelling, testing and design of gradient-CVI derived CMC components. AGARD Report 795. Introduction of Ceramics into Aerospace Structural Composites, 1993, pp. 14-1.
2. Mühlratzer, A., Agatonovic, P. et al., in Advanced structural fiber composites, ed. P. Vincenzini. Techna Srl., 1995.
3. Köberle, H. et al., in Ceramic processing science and technology, 51. American Ceramic Society, 1995, pp. 249-53.
4. Than, E., Mühlratzer, A. and Kudela, S., in Symposium Verbundwerkstoffe und Werksloffverbunde. (Bayreuth, Germany), In press.
5. Auweter-Kurtz, M. et al., in First European Symposium on Aerothermodynamics for Space Vehicles. (Nordwijk, Netherlands), 1991.
6. Loesener, O. et al., in AIAA 26th Thermophysics Conference. (Honolulu, Hawaii), 1991.
7. Krenkel, W., in 40th International Astronautical Congress (IAF). (Malaga, Spain), 1989.