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Fabrication and Testing of a Leading-Edge-Shaped Heat Pipe
Author(s) -
David E. Glass,
Charles J. Camarda,
Michael A. Merrigan,
J.T. Sena,
Robert S. Reid
Publication year - 1999
Publication title -
journal of spacecraft and rockets
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.758
H-Index - 79
eISSN - 1533-6794
pISSN - 0022-4650
DOI - 10.2514/2.3515
Subject(s) - spacecraft , aerospace engineering , missile , space (punctuation) , systems engineering , spacecraft design , mechanical engineering , space technology , space research , heat shield , engineering , computer science , operating system
The development of a refractory-composite/heat-pipe-cooled leading edge has evolved from the design stage to the fabrication and testing of a full size, leading-edge-shaped heat pipe. The heat pipe had a D-shaped cross section and was fabricated from arc cast Mo-41Re. An artery was included in the wick. Several issues were resolved with the fabrication of the sharp leading edge radius heat pipe. The heat pipe was tested in a vacuum chamber at Los Alamos National Laboratory using induction heating and was started up from the frozen state several times. However, design temperatures and heat fluxes were not obtained due to premature failure of the heat pipe resulting from electrical discharge between the induction heating apparatus and the heat pipe. Though a testing anomaly caused premature failure of the heat pipe, successful startup and operation of the heat pipe was demonstrated.

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