Life prediction of thermally highly loaded components: modelling the damage process of a rocket combustion chamber hot wall

Author:

Schwarz W.,Schwub S.,Quering K.,Wiedmann D.,Höppel H. W.,Göken M.

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Aerospace Engineering

Reference52 articles.

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3. Jain, P., Raj, S.V., Hemker, H.J.: Characterization of nicraly coatings for a high strength, high conductivity grcop-84 copper alloy. Acta Mater. 55, 5103–5113 (2007)

4. “Advanced high pressure O2/H2 technology”. Technical Report, NASA-CP-2372, NASA (1984)

5. Hannum, N.P., Kasper, H.J., Pavli, A.J.: Experimental and theoretical investigation of fatigue life in reusable rocket thrust chambers. Technical Report, NASA TM-X-73413, NASA (1976)

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