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the claim

Liquid propellant rocket engines experience thrust oscillation during operation

the verdict

SUPPORTED

the evidence backs this

confidence 77/100

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

Evidence for · 2

Experimental Study on the Unsteady Spray Combustion Process of a Liquid Oxygen/Methane Swirl Coaxial Injector.

2021 · cited by 1

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

Bio-inspired multi-dimensional deep fusion learning for predicting dynamical aerospace propulsion systems.

2024 · cited by 0

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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