Experimental Characterization and CFD Validation of Liquid–Liquid Pintle Injector Spray Patterns Using Water as Simulant
Jamakeyev I. Stepanov S. Khamzatov D. Zhunusov R. Tleukhabylova Y. Beisenov A. Nurguzhin M. Omarbayev M.
February 2026Multidisciplinary Digital Publishing Institute (MDPI)
Aerospace
2026#13Issue 2
Pintle injectors offer variable thrust capability and combustion stability advantages for liquid rocket engines. This study presents experimental and numerical investigation of spray characteristics for a liquid–liquid pintle injector using water as simulant. Ten cold flow tests covering total momentum ratio (TMR) from 0.36 to 2.76 captured spray angle variations from 26° to 80°. Computational fluid dynamics (CFD) simulations using Ansys Fluent 2025 R1 with the Volume of Fluid method and dispersed interface modeling showed good agreement with experimental spray angles for TMR > 0.74 (error < 8%), but demonstrated increasing discrepancy at lower TMR values (up to 62% error at TMR = 0.36). This deviation indicates limitations of steady-state RANS models in capturing unsteady, fuel-dominated flow regimes. The experimental dataset provides validation benchmarks for CFD modeling and contributes to injector design optimization for sounding rocket applications.
CFD validation , cold flow testing , liquid rocket engine , pintle injector , spray characterization , total momentum ratio
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JSC National Centre for Space Research and Technology, Almaty, 050010, Kazakhstan
LLC Thrust, Almaty, 050010, Kazakhstan
JSC National Centre for Space Research and Technology
LLC Thrust
10 лет помогаем публиковать статьи Международный издатель
Книга Публикация научной статьи Волощук 2026 Book Publication of a scientific article 2026