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the claim

Alternative bearings such as hydrostatic gas bearings are studied for rocket turbopumps

the verdict
SUPPORTED
the evidence backs this
Recorded sources
5 sources for · 0 against

Counts group repeated records of the same source within each side. They do not measure evidence strength or source independence.

Is it true that alternative bearings such as hydrostatic gas bearings are studied for rocket turbopumps?

Yes. Multiple studies demonstrate that alternative bearings, specifically hydrostatic and hybrid gas or fluid film bearings, are actively studied and designed for use in rocket engine turbopumps to handle extreme cryogenic conditions and improve reliability.

Verdict: SUPPORTED · 5 sources for, 0 against · Last checked

The analysis

The claim asserts that alternative bearings such as hydrostatic gas bearings are studied for rocket turbopumps. Multiple provided papers (e.g., [0], [2], [4], [6], [8]) explicitly investigate hydrostatic and hybrid bearings for cryogenic rocket engine turbopumps, demonstrating clear and unequivocal support with no refutations in the provided literature.

Evidence for · 5
1969
Analyzes hydrostatic bearings for use in high-pressure cryogenic rocket engine turbopumps.
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Reddecliff, J. M. & Vohr, J. H. (1969). Hydrostatic Bearings for Cryogenic Rocket Engine Turbopumps. doi.org. https://doi.org/10.1115/1.3554989

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More for · 4
2022
Discusses hydrostatic bearings for liquid rocket engine turbopumps providing distinctive advantages.
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Yi, H., Jung, H., Kim, K., & Ryu, K. (2022). Static Load Characteristics of Hydrostatic Journal Bearings: Measurements and Predictions. doi.org. https://doi.org/10.3390/s22197466

2023
Notes that turbopumps in reusable and low-cost liquid rocket engines require hydrostatic bearings.
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Jung, H., Kim, K., & Ryu, K. (2023). On The Performance Of Hydrostatic Journal Bearings In Air, Water, And Liquid Nitrogen: Measurements And Predictions. doi.org. https://doi.org/10.1115/1.4063282

2014
Examines hybrid bearings in advanced cryogenic rocket engine turbopumps operating under liquid oxygen.
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Guoyuan, Z. & Xiu-Tian, Y. (2014). Analysis of two phase flow in liquid oxygen hybrid journal bearings for rocket engine turbopumps. doi.org. https://doi.org/10.1108/ilt-09-2011-0072

2026
Presents a performance analysis of a hybrid tilting pad journal bearing for reusable liquid methane turbopumps.
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Y, K. & TH, K. (2026). Predictions of Liquid Methane (LCH<sub>4</sub>) Lubricated Hybrid Tilting Pad Journal Bearings for Reusable Rocket Turbopumps.. doi.org. https://doi.org/10.3390/ma19112285

What does the evidence say?

The claim asserts that alternative bearings such as hydrostatic gas bearings are studied for rocket turbopumps. Multiple provided papers (e.g., [0], [2], [4], [6], [8]) explicitly investigate hydrostatic and hybrid bearings for cryogenic rocket engine turbopumps, demonstrating clear and unequivocal support with no refutations in the provided literature.

Receipt History
first checked05 Aug 2026
judged → SUPPORTED · 8605 Aug 2026
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