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Effects of atomic oxygen on graphite ablationIt is shown that a previously derived semiempirical equation for describing observed ablation rates of isotropic graphites cannot be applied to low-density flows containing dissociated oxygen. Experimentally determined reaction probabilities of isotropic graphites to molecular and atomic oxygen are used to calculate heat-transfer rates and stagnation-point ablation rates for typical conditions. Integrated mass losses are computed for a group of flight trajectories which start from geosynchronous orbit and enter earth's atmosphere in a skipping motion following near-elliptic decaying orbits. A comparison of the results with those obtained by the equation under question shows excellent agreement for steep trajectories, but large discrepancies for shallow trajectories. The differences are attributed to surface oxidation by atomic oxygen.
Document ID
19770030871
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Park, C.
(NASA Ames Research Center Moffett Field, Calif., United States)
Date Acquired
August 9, 2013
Publication Date
November 1, 1976
Publication Information
Publication: AIAA Journal
Volume: 14
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
77A13723
Distribution Limits
Public
Copyright
Other

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