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The theoretical treatment of cooling processes in porous rocket thrustchambers

  1. Said Ghadiani1,
  2. Wolfgang Ehlers2

Article first published online: 24 NOV 2004

DOI: 10.1002/pamm.200410109

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PAMM

PAMM

Volume 4, Issue 1, pages 256–257, December 2004

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How to Cite

Ghadiani, S. and Ehlers, W. (2004), The theoretical treatment of cooling processes in porous rocket thrustchambers. Proc. Appl. Math. Mech., 4: 256–257. doi: 10.1002/pamm.200410109

Author Information

  1. 1

    Institute of Structures and Design (Space Structural Components), German Aerospace Center, DLR Stuttgart, www.st.dlr.de/bk

  2. 2

    Institute of Applied Mechanics (CE), University of Stuttgart, Pfaffenwaldring 7, 70569 Stuttgart, Germany, www.mechbau.uni-stuttgart.de/ls2

Publication History

  1. Issue published online: 24 NOV 2004
  2. Article first published online: 24 NOV 2004

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References

  • [1]
    E. Serbest, Untersuchungen zur Anwendung der Effusionskühlung bei Raketenbrennkammern (Ph.D. thesis), RWTH-Aachen (2002).
  • [2]
    NASA/SP-8087, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical), NASA Lewis Research Center (Cleveland, 1972).
  • [3]
    T. Ullman and H. Hald, Behaviour of C/C-Sic Materials in Reentry, Workshop on Thermal Protecting Systems, Netherlands (1998).
  • [4]
    W. Ehlers and J. Bluhm (eds.), Porous Media: Theory, Experiments and Numerical Applications, Springer-Verlag, Berlin (2002).
  • [5]
    S. Ghadiani, A Multiphasic Continuum Mechanical Model for the Theoretical Investigation of an Effusion Cooled Rocket Thrust Chamber (Ph.D. thesis), University of Stuttgart (submitted 2004).
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