Create propulsion_system.cpp

core/aerospace/propulsion_system.cpp

@@ -0,0 +1,33 @@
+#include <iostream>
+#include <cmath>
+
+class PropulsionSystem {
+public:
+    PropulsionSystem(double thrust, double specific_impulse) {
+        this->thrust = thrust;
+        this->specific_impulse = specific_impulse;
+    }
+
+    double calculate_acceleration(double mass) {
+        return this->thrust / mass;
+    }
+
+    double calculate_delta_v(double mass, double time) {
+        return this->thrust / mass * time;
+    }
+
+private:
+    double thrust;
+    double specific_impulse;
+};
+
+int main() {
+    PropulsionSystem propulsion_system(100, 300);
+    double mass = 1000;
+    double time = 10;
+    double acceleration = propulsion_system.calculate_acceleration(mass);
+    double delta_v = propulsion_system.calculate_delta_v(mass, time);
+    std::cout << "Acceleration: " << acceleration << " m/s^2" << std::endl;
+    std::cout << "Delta-v: " << delta_v << " m/s" << std::endl;
+    return 0;
+}