The EXPERT C/C-SiC nose cap - System design and thermomechanical layout

A Collection of Technical Papers - 13th AIAA/CIRA International Space Planes and Hypersonic Systems and Technologies Conference

Volumn 1, Issue , 2005, Pages 556-563

  Reimer, Thomas ^a,b  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

^b UNIVERSITY OF STUTTGART   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; INTERFACES (MATERIALS); REENTRY; SYSTEMS ANALYSIS; THERMAL LOAD; THERMOMECHANICAL TREATMENT;

IN-FLIGHT DATA; RE-ENTRY VEHICLES; THERMAL PROTECTION SYSTEMS (TPS); THERMOMECHANICAL LAYOUTS;

FLIGHT DYNAMICS;

EID: 29044439088     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (7)

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3. Laux, T., Untersuchungen zur Hochtemperaturoxidation von Siliziumkarbid in Plasmaströmungen, Dissertation, Institute of Space Systems, Stuttgart University, Germany, 2004
4. Heuer, A. H., and Lou, V. L.K., Volatility Diagrams for Silica, Silicon Nitride, and Silicon Carbide and Their Application to High-Temperature Decomposition and Oxidation, J. Am. Ceram. Soc, 1990, Vol.73, 10, 2789-2803
5. Curry, D. M., Space Shuttle Orbiter Thermal Protection System Design and Flight Experience, 1st ESA/ESTEC Workshop on Thermal Protection Systems, 1993, Noordwijk, ESA/ESTEC
6. Tigges, M., Preliminary V-201 Entry Flight Profile with Landing Site Precision. Cycle 8, NASA, 1998, October, Technical Report
7. Voinov, L.P., Thermal Designing of the BURAN Orbital Spaceship, Aerospace Systems: Book of Technical Papers, 1997, 115-122, Lozino-Lozinsky, G.E., Bratukhin, A.G., Publishing House of Moscow Aviation Institute, Moscow