Sofyan S, Wuwung V. RX-320 Rocket Static Pressure Combustion Chamber Prediction and Validation by Using Invers Method. Indonesian Journal of Aerospace [Internet]. 2018 Sep. 17 [cited 2025 Dec. 6];16(1 Juni):45-58. Available from: https://ejournal.brin.go.id/ijoa/article/view/12302