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] Filters: Keyword is high-frequency combustion instability; liquid propellant rocket engine; aerospike; oxygen/methane; natural oscillation modes; pressure oscillation decrement; hot-fire tests [Clear All Filters]
. High-frequency stability analysis of an aerospike rocket engine taking into account interaction of acoustics and vibrations of toroidal chamber structure. Space Science and Technology. 2026 ;32(1):13-26.