1996
DOI: 10.1080/10426919608947492
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Advanced HfC-TaC Oxidation Resistant Composite Rocket Thruster

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Cited by 32 publications
(16 citation statements)
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“…Since tantalum oxide stabilizes tetragonal hafnia, it is useful during cooling in order to prevent the tetragonal/monoclinic transition at about 1750°C. Indeed, this transition is accompanied by a 3.5% volume increase and results in the formation of cracks in the coating [1][2][3].…”
Section: Introductionmentioning
confidence: 98%
“…Since tantalum oxide stabilizes tetragonal hafnia, it is useful during cooling in order to prevent the tetragonal/monoclinic transition at about 1750°C. Indeed, this transition is accompanied by a 3.5% volume increase and results in the formation of cracks in the coating [1][2][3].…”
Section: Introductionmentioning
confidence: 98%
“…However, coating suffers from several disadvantages such as easily appeared cracks due to CTE mismatch with substrate; and doping only provides good protection up to 700°C. That leaves carbon fibers reinforced ceramic composite as the most promising material [11][12][13][14][15].…”
Section: Introductionmentioning
confidence: 99%
“…Currently, there is a good deal of interest in HfC for rocket thrusters (Patterson, 1996). Shimada et al (1997) have examined the oxidation of HfC from 600 to 900°C.…”
Section: Transition Metal Carbidesmentioning
confidence: 99%
“…These materials are under consideration for rocket thrusters (Patterson et al, 1996) and ZrC is important in nuclear applications (Rama Rao and Venugopal, 1994). …”
Section: Transition Metal Carbidesmentioning
confidence: 99%