Secure tightening of a CMC fastener for the heat shield of re-entry vehicles

Author:

Böhrk H.,Beyermann U.

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference25 articles.

1. Hypersonic and high temperature gas dynamics;Anderson,1989

2. CMC materials: from plasma channel testing to real capsule re-entry;Hald;High Temp Chem Process,1994

3. Hald H. 2001. Faserkeramiken für heiße Strukturen von Wiedereintrittsfahrzeugen – Simulation, Test und Vergleich mit experimentellen Flugdaten. PhD-thesis, Universität Stuttgart.

4. Reimer T. The KERAMIK thermal protection system experiment on the FOTON-M2 Mission. In: Proceedings of the 5th European workshop on thermal protection systems and hot structures (SP-631). Noordwijk. The Netherlands; May 2006.

5. Eggers T, Longo J, Turner J, Jung W, Hörschgen M, Stamminger A, et al. The SHEFEX flight experiment – pathfinder experiment a for a sky based test facility. In: Proceedings of the 14th AIAA spaceplane systems and technologies conference. Canberra, Australia; Nov 2006.

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