Experimental investigation on IXV TPS interface effects in Plasmatron

Author:

Ceglia Giuseppe,Trifoni Eduardo,Gouriet Jean-Baptiste,Chazot Olivier,Mareschi Vincenzo,Rufolo Giuseppe,Tumino Giorgio

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Aerospace Engineering

Reference10 articles.

1. Rakich, J.V., Stewart, D.A., Lanfranco, M.J.: Results of a flight experiment on the catalytic efficiency of the space shuttle heat shield. AIAA Pap. 81, 0944 (1982)

2. Anderson, J.D.: Hypersonic and High Temperature Gas Dynamics. McGraw Hill, New York (1989)

3. Panerai, F.: Aerothermochemistry characterization of thermal protection systems. Dissertation, Ph.D. thesis, Università degli Studi di Perugia, von Kármán Institute for Fluid Dynamics (2012)

4. Panerai, F., Chazot, O.: Plasma wind tunnel testing as support to the design of gas-surface interaction in-flight experiments. In: Proceedings of 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, AIAA 2011–2276, San Francisco, CA, USA (2011)

5. Bottin, B., Carbonaro, M., Zemsch, S., Degrez, G.: Aerothermodynamic design of an inductively-coupled plasma wind tunnel. In: Proceedings of 32nd Thermophysics Conference, AIAA 97–2498, Atlanta, USA (1997)

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