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the claim

Liquid propellant rocket engines experience thrust oscillation during operation

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

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

Liquid propellant rocket engines frequently experience combustion instabilities and thrust oscillations during operation, as documented in experimental and modeling studies.

The analysis

The retrieved papers include direct empirical evidence (Paper 5) and discussions of combustion instability (Paper 9) in liquid rocket engines, confirming that liquid propellant engines experience these oscillations.

Evidence for · 2
Recorded source metadata

Cao P, Bai X, Li Q, Cheng P, Li Z. Experimental Study on the Unsteady Spray Combustion Process of a Liquid Oxygen/Methane Swirl Coaxial Injector.. 2021. https://doi.org/10.1021/acsomega.1c03192

Experimental results on a liquid oxygen/methane rocket engine confirm the presence of low-frequency and high-frequency flame and spray oscillations during combustion operations.

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More for · 1
Recorded source metadata

Vergnolle MQ, Wu EZY, Sui Y, Wang Q. Bio-inspired multi-dimensional deep fusion learning for predicting dynamical aerospace propulsion systems.. 2024. https://doi.org/10.1038/s44172-024-00327-9

Discusses rocket combustion instability as a key dynamical challenge in aerospace propulsion systems.

The paper trail · every fact has a biography
first checked01 Aug 2026
judged → SUPPORTED · 7701 Aug 2026
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