35th Congress of the International Council of the Aeronautical Sciences

05 - Propulsion and Energy

ACTIVE THRUST BALANCING CONTROL OF A TURBOPUMP WITH A SWIRL BREAKER

S.M. Jeon, Korea Aerospace Research Institute, South Korea

An active balancing system is applied for aircraft and rocket engine turbopump thrust control, with a swirl breaker configured to enhance control ability. To obtain the optimal design through numerical analysis, a parameter study was conducted using an in-house developed reduced-order computer program.


View Paper

DOI: 10.71945/icas2026_0024