Work

A Bernoulli featured GRU flow sensor for propellant flowrate and mixture ratio estimation in transient phase of liquid propellant rocket engine with SHAP-Interpretability

Year: 2026

Type: article

Source: Aerospace Science and Technology

DOI: 10.1016/j.ast.2026.113700

Authors: Anisha Selva Kala R, Jeraldin Auxillia D, Jessi Flora J․

Institutions: Loyola Institute of Technology and Science, Indian Space Research Organisation, ISRO Propulsion Complex

Language: English

Topic: Rocket and propulsion systems research

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

OpenAlex ID: W7204697133

FWCI:

Cites: 40

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Related to: 10