View of OPTIMIZING CONVERGENT-DIVERGENT ROCKET NOZZLE GEOMETRY (30°/10°) TO ENHANCE THE ALTITUDE PERFORMANCE OF MODEL ROCKETS USING SOLID SUGAR PROPELLANTS

Return to Article Details OPTIMIZING CONVERGENT-DIVERGENT ROCKET NOZZLE GEOMETRY (30°/10°) TO ENHANCE THE ALTITUDE PERFORMANCE OF MODEL ROCKETS USING SOLID SUGAR PROPELLANTS Download Download PDF