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High Temperature Material Processes: An International Quarterly of High-Technology Plasma Processes

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ISSN Druckformat: 1093-3611

ISSN Online: 1940-4360

The Impact Factor measures the average number of citations received in a particular year by papers published in the journal during the two preceding years. 2017 Journal Citation Reports (Clarivate Analytics, 2018) IF: 0.4 The Immediacy Index is the average number of times an article is cited in the year it is published. The journal Immediacy Index indicates how quickly articles in a journal are cited. Immediacy Index: 0.1 The Eigenfactor score, developed by Jevin West and Carl Bergstrom at the University of Washington, is a rating of the total importance of a scientific journal. Journals are rated according to the number of incoming citations, with citations from highly ranked journals weighted to make a larger contribution to the eigenfactor than those from poorly ranked journals. Eigenfactor: 0.00005 The Journal Citation Indicator (JCI) is a single measurement of the field-normalized citation impact of journals in the Web of Science Core Collection across disciplines. The key words here are that the metric is normalized and cross-disciplinary. JCI: 0.07 SJR: 0.198 SNIP: 0.48 CiteScore™:: 1.1 H-Index: 20

Indexed in

POST-FLIGHT ANALYSES OF THE OREX CATALYCITY EXPERIMENT

Volumen 9, Ausgabe 3, 2005, pp. 353-361
DOI: 10.1615/HighTempMatProc.v9.i3.30
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ABSTRAKT

Catalytic recombination of dissociated atmospheric oxygen and nitrogen is a major heat source for re-entry vehicles beyond Mach 10. Present thermal protection systems are designed to the extreme assumption of full catalycity. However mass, performance, and cost considerations of future reusable launch vehicles require that their thermal protection system is designed to the more realistic assumption of partial catalycity. With this in mind, the authors of this paper have studied the catalytic behavior of a coated C/C material as it was used for the heat shield of the OREX re-entry capsule. In this presentation, we will report on the laboratory measurements of the atomic oxygen recombination coefficient and its associated coefficient for thermal accommodation. The recombination coefficient was determined in plasma test chambers by actinometry and in plasmatron at 200 and 2000 Pa, respectively. The results show an effective recombination coefficient of the order of 1% (600 K - 1900 K). Unlike Stewart and the Bruno models, we did not observe a strong temperature dependency of the effective recombination coefficient, neither in the laboratory data nor in the flight data. The observed behaviour can be explained by the Cacciatore model on silica.

REFERENZIERT VON
  1. Da Rold Guillaume, Guyon Cédric, Cavadias Siméon, Amouroux Jacques, Barriers of Oxidation ans Ageing of Space Shuttle Material, Advanced Materials Research, 89-91, 2010. Crossref

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