Sugestions Update

Sugestions made by @phmbressan implemented

Author: caioessouza

CHANGELOG.md

@@ -32,8 +32,6 @@ Attention: The newest changes should be on top -->
 
 ### Added
 - ENH: Enable only radial burning [#815](https://github.com/RocketPy-Team/RocketPy/pull/815)
-- ENH: Controller (AirBrakes) and Sensors Encoding [#849] (https://github.com/RocketPy-Team/RocketPy/pull/849)
-- EHN: Addition of ensemble variable to ECMWF dictionaries [#842] (https://github.com/RocketPy-Team/RocketPy/pull/842) 
 - ENH: Tank Fluids with Variable Density from Temperature and Pressure [#852](https://github.com/RocketPy-Team/RocketPy/pull/852)
 - ENH: Controller (AirBrakes) and Sensors Encoding [#849](https://github.com/RocketPy-Team/RocketPy/pull/849)
 - EHN: Addition of ensemble variable to ECMWF dictionaries [#842](https://github.com/RocketPy-Team/RocketPy/pull/842) 
@@ -479,4 +477,4 @@ You can install this version by running `pip install rocketpy==1.0.1`
 ### Fixed
 
 - BUG: Remove NoseCone Warning [#428](https://github.com/RocketPy-Team/RocketPy/pull/428)
-- BUG: motor coordinates [#423](https://github.com/RocketPy-Team/RocketPy/pull/423)
+- BUG: motor coordinates [#423](https://github.com/RocketPy-Team/RocketPy/pull/423)

rocketpy/motors/hybrid_motor.py

@@ -193,8 +193,11 @@ class HybridMotor(Motor):
     HybridMotor.reference_pressure : int, float
         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). 
+        Grain length remains constant throughout the burn. Default is False.
+    """    
+    # pylint: disable=too-many-arguments
     def __init__(  # pylint: disable=too-many-arguments
         self,
         thrust_source,
@@ -314,6 +317,11 @@ class Function. Thrust units are Newtons.
             "nozzle_to_combustion_chamber".
         reference_pressure : int, float, optional
             Atmospheric pressure in Pa at which the thrust data was recorded.
+        only_radial_burn : boolean, optional
+            If True, inhibits the grain from burning axially, only computing
+            radial burn. If False, allows the grain to also burn
+            axially. May be useful for axially inhibited grains or hybrid motors.
+            Default is False.
 
         Returns
         -------

rocketpy/motors/solid_motor.py

@@ -193,8 +193,10 @@ class SolidMotor(Motor):
     SolidMotor.reference_pressure : int, float
         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). 
+        Grain length remains constant throughout the burn. Default is False.
     """
-
     # pylint: disable=too-many-arguments
     def __init__(
         self,
@@ -413,6 +415,10 @@ 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
 
     @property
     def propellant_initial_mass(self):

tests/unit/test_solidmotor.py

@@ -282,7 +282,15 @@ def test_reshape_thrust_curve_asserts_resultant_thrust_curve_correct(
 
 
 def test_only_radial_burn_parameter_effect(cesaroni_m1670):
-    # Tests if the only_radial_burn flag is properly set
+    """Tests the effect of the only_radial_burn parameter on burn area
+    calculation. When enabled, the burn area should only account for
+    the radial surface of the grains (no axial regression).
+
+    Parameters
+    ----------
+    cesaroni_m1670 : rocketpy.SolidMotor
+        The SolidMotor object used in the test.
+    """
     motor = cesaroni_m1670
     motor.only_radial_burn = True
     assert motor.only_radial_burn is True
@@ -298,7 +306,15 @@ def test_only_radial_burn_parameter_effect(cesaroni_m1670):
 
 
 def test_evaluate_geometry_updates_properties(cesaroni_m1670):
-    # Checks if after instantiation, grain_inner_radius and grain_height are valid functions
+    """Tests if the grain geometry evaluation correctly updates SolidMotor
+    properties after instantiation. It ensures that grain geometry
+    functions are created and behave as expected.
+
+    Parameters
+    ----------
+    cesaroni_m1670 : rocketpy.SolidMotor
+        The SolidMotor object used in the test.
+    """
     motor = cesaroni_m1670
 
     assert hasattr(motor, "grain_inner_radius")