2011
DOI: 10.3367/ufne.0181.201103f.0319
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Selecting and using materials for a nuclear rocket engine reactor

Abstract: This paper provides a historical account of how the nuclear rocket engine reactor was created and discusses the problem of selecting materials for a gas environment at the temperature up to 3100 K and energy release 30 MW per liter.

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Cited by 12 publications
(2 citation statements)
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“…For example, the fuel rod length in the proposed TWR variant (see the "ideal" case in Table1) is predetermined by the nuclear burning wave speed, which in a given case equals to 0.254 cm/day≡ 85 cm/year, i.e. 20 years of TWR operation requires the fuel rod length ∼ 17 m. On the other hand, it is known [78] that for a twisted fuel rod form with two-or four-bladed symmetry, the tension emerging from the fuel rod surface cooling is 30% lower than that of a round rod with the same diameter, other conditions being equal. The same reduction effect applies to the hydraulic resistance in comparison to a round rod of the same diameter.…”
Section: Discussionmentioning
confidence: 99%
“…For example, the fuel rod length in the proposed TWR variant (see the "ideal" case in Table1) is predetermined by the nuclear burning wave speed, which in a given case equals to 0.254 cm/day≡ 85 cm/year, i.e. 20 years of TWR operation requires the fuel rod length ∼ 17 m. On the other hand, it is known [78] that for a twisted fuel rod form with two-or four-bladed symmetry, the tension emerging from the fuel rod surface cooling is 30% lower than that of a round rod with the same diameter, other conditions being equal. The same reduction effect applies to the hydraulic resistance in comparison to a round rod of the same diameter.…”
Section: Discussionmentioning
confidence: 99%
“…The components of the reactor/thermally driven carbon dioxide laser are the high temperature core, the nitrogen flow channels and the laser/mixing cavity. The reactor fuels that were examined for the high temperature core were ZrC, UC and NbC (Table 5.20) based on their potential operating temperatures of 2000 K and beyond [84]. The second part of the design was the flow of nitrogen gas from the reactor core to the laser cavity.…”
mentioning
confidence: 99%