diff --git a/CHANGELOG.md b/CHANGELOG.md
index 0d168763a..2e8635f16 100644
--- a/CHANGELOG.md
+++ b/CHANGELOG.md
@@ -36,6 +36,7 @@ Attention: The newest changes should be on top -->
 
 ### Changed
 
+- DOCS: reshape docs (closes #659) [#781](https://github.com/RocketPy-Team/RocketPy/pull/781)
 - MNT: EmptyMotor class inherits from Motor(ABC) [#779](https://github.com/RocketPy-Team/RocketPy/pull/779)
 
 ### Fixed
diff --git a/docs/user/motors/thrust.rst b/docs/user/motors/thrust.rst
index cbe327032..4359023b6 100644
--- a/docs/user/motors/thrust.rst
+++ b/docs/user/motors/thrust.rst
@@ -164,6 +164,8 @@ class also supports them. Let's see how to use it.
     )
     solid_lambda.info()
 
+.. _reshaping_thrust_curve:
+
 Reshaping and interpolating the thrust curve
 --------------------------------------------
 
diff --git a/rocketpy/motors/motor.py b/rocketpy/motors/motor.py
index cad0a60f4..5f4b0dc0b 100644
--- a/rocketpy/motors/motor.py
+++ b/rocketpy/motors/motor.py
@@ -878,7 +878,8 @@ def propellant_I_23(self):
     def reshape_thrust_curve(thrust, new_burn_time, total_impulse):
         """Transforms the thrust curve supplied by changing its total
         burn time and/or its total impulse, without altering the
-        general shape of the curve.
+        general shape of the curve. This method does not mutate the original
+        object, it only returns a new thrust curve.
 
         Parameters
         ----------
@@ -893,6 +894,10 @@ def reshape_thrust_curve(thrust, new_burn_time, total_impulse):
         -------
         Function
             Reshaped thrust curve.
+
+        Tip
+        ---
+        See the User Guide page for examples on how to use this method.
         """
         # Retrieve current thrust curve data points
         time_array, thrust_array = thrust.x_array, thrust.y_array