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Design and experimental investigation of twin rockets embedded in the strut for RBCC

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Experimental study demonstrates high combustion efficiency and reliable ignition in strut rockets, indicating robust thermal protection.

Combustion efficiency of the strut rocket reached 97.8%, showcasing excellent performance.
Experimental tests confirmed reliable ignitions and no throat ablation in the thrust chamber.
Design included cooling channels and thorough evaluations of injector and thermal protection systems.
Study aligns with RBCC engine requirements, ensuring effective gas-liquid propellant mixing.

Qu et al. (2025) studied this question.

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