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Author

Insang Moon

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Open access Aug 2026

Tank Head Startup Analysis of a Gas Generator Cycle Liquid Rocket Engine

Startup transients are critical in gas generator cycle liquid rocket engines because pressure overshoot, mixture-ratio excursions, and turbopump instability can occur before steady operation. This study compares conventional pyrostarter and tank head start sequences using a system-level transient model of propellant fe...

S. Yoon, Insang Moon · 1 citation

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