ENH: capitalize words on prints

Author: Lucas-Prates

rocketpy/prints/hybrid_motor_prints.py

@@ -77,7 +77,7 @@ def motor_details(self):
         print(
             f"Total Propellant Mass: {self.hybrid_motor.propellant_initial_mass:.3f} kg"
         )
-        print(f"Structural to total mass ratio: {self.hybrid_motor.structural_mass_ratio:.3f}")
+        print(f"Structural Mass Ratio: {self.hybrid_motor.structural_mass_ratio:.3f}")
         avg = self.hybrid_motor.exhaust_velocity.average(*self.hybrid_motor.burn_time)
         print(f"Average Propellant Exhaust Velocity: {avg:.3f} m/s")
         print(f"Average Thrust: {self.hybrid_motor.average_thrust:.3f} N")

rocketpy/prints/liquid_motor_prints.py

@@ -47,7 +47,7 @@ def motor_details(self):
         print(
             f"Total Propellant Mass: {self.liquid_motor.propellant_initial_mass:.3f} kg"
         )
-        print(f"Structural to total mass ratio: {self.liquid_motor.structural_mass_ratio:.3f}")
+        print(f"Structural Mass Ratio: {self.liquid_motor.structural_mass_ratio:.3f}")
         avg = self.liquid_motor.exhaust_velocity.average(*self.liquid_motor.burn_time)
         print(f"Average Propellant Exhaust Velocity: {avg:.3f} m/s")
         print(f"Average Thrust: {self.liquid_motor.average_thrust:.3f} N")

rocketpy/prints/motor_prints.py

@@ -35,7 +35,7 @@ def motor_details(self):
         print("Motor Details")
         print("Total Burning Time: " + str(self.motor.burn_out_time) + " s")
         print(f"Total Propellant Mass: {self.motor.propellant_initial_mass:.3f} kg")
-        print(f"Structural to total mass ratio: {self.motor.structural_mass_ratio:.3f}")
+        print(f"Structural Mass Ratio: {self.motor.structural_mass_ratio:.3f}")
         print(
             "Average Propellant Exhaust Velocity: "
             f"{self.motor.exhaust_velocity.average(*self.motor.burn_time):.3f} m/s"

rocketpy/prints/solid_motor_prints.py

@@ -65,7 +65,7 @@ def motor_details(self):
         print(
             f"Total Propellant Mass: {self.solid_motor.propellant_initial_mass:.3f} kg"
         )
-        print(f"Structural to total mass ratio: {self.solid_motor.structural_mass_ratio:.3f}")
+        print(f"Structural Mass Ratio: {self.solid_motor.structural_mass_ratio:.3f}")
         average = self.solid_motor.exhaust_velocity.average(*self.solid_motor.burn_time)
         print(f"Average Propellant Exhaust Velocity: {average:.3f} m/s")
         print(f"Average Thrust: {self.solid_motor.average_thrust:.3f} N")