Surface characterization of metallic and ceramic TPS-materials for reusable space vehicles

Author:

Schüßler M.,Auweter-Kurtz M.,Herdrich G.,Lein S.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference30 articles.

1. M. Heilmaier, F.E.H. Müller, The role of grain structure in the creep and fatigue of Ni-based super alloy PM1000, JOM, A publication of the Minerals, Metals & Materials Society, vol. 51, April 1999.

2. M. Heilmaier, H.J. Maier, A. Jung, M. Nganbe, F.E.H. Müller, H.-J. Christ, Cyclic stress–strain response of the ODS nickel-base, super alloy PM 1000 under variable amplitude loading at high temperatures, Materials Science and Engineering A 281 (2000).

3. J. Offerman, S. Birjmohan, G. Kester, G. Ramusat, Reusable high temperature resistant metallic control surface for RLV application, IAC-04-IAF-V.5.02, 2004.

4. J. Fatemi, S. Birjmohan, M. Rijkeboer, M.C.M. Bakker, Analysis and testing of a metallic thermal protection system for RLV application, in: 4th International Symposium Atmospheric Re-entry Vehicles and Systems, March 2005.

5. A.F. Kolesnikov, Combined measurements and computations of high enthalpy and plasma flows for determination of TPM surface catalycity, RTO AVT/VKI Special Course on “Measurement Techniques for High Enthalpy Plasma Flows”, von Karman Institute for Fluid Dynamics, RTO EN-1, Rhode-Saint-Genèse, Belgium, Okt, 1999.

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