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