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Code formated using ruff

Author: caioessouza

rocketpy/motors/hybrid_motor.py

@@ -194,9 +194,10 @@ class HybridMotor(Motor):
         Atmospheric pressure in Pa at which the thrust data was recorded.
         It will allow to obtain the net thrust in the Flight class.
     SolidMotor.only_radial_burn : bool
-        If True, grain regression is restricted to radial burn only (inner radius growth). 
+        If True, grain regression is restricted to radial burn only (inner radius growth).
         Grain length remains constant throughout the burn. Default is False.
-    """    
+    """
+
     # pylint: disable=too-many-arguments
     def __init__(  # pylint: disable=too-many-arguments
         self,

rocketpy/motors/solid_motor.py

@@ -194,9 +194,10 @@ class SolidMotor(Motor):
         Atmospheric pressure in Pa at which the thrust data was recorded.
         It will allow to obtain the net thrust in the Flight class.
     SolidMotor.only_radial_burn : bool
-        If True, grain regression is restricted to radial burn only (inner radius growth). 
+        If True, grain regression is restricted to radial burn only (inner radius growth).
         Grain length remains constant throughout the burn. Default is False.
     """
+
     # pylint: disable=too-many-arguments
     def __init__(
         self,
@@ -415,7 +416,7 @@ def exhaust_velocity(self):
         return Function(
             self.total_impulse / self.propellant_initial_mass
         ).set_discrete_based_on_model(self.thrust)
-    
+
     @property
     def only_radial_burn(self):
         return self._only_radial_burn