Regression analysis on the selection of hybrid rocket engine with suitable nano–additives

Puntos clave

• Performance optimization revealed a significant relationship between nano-additives and propulsion efficiency.
• Regression analysis indicated that specific nano-additives can enhance combustion stability and thrust.
• The approach assessed various propellant characteristics to identify ideal combinations with nano-additives.
• Findings support further exploration of nano-additives in hybrid rocket design for increased performance.