diff --git a/CHANGELOG.md b/CHANGELOG.md
index 4c3aa2373..19510c92d 100644
--- a/CHANGELOG.md
+++ b/CHANGELOG.md
@@ -45,6 +45,7 @@ Attention: The newest changes should be on top -->
 
 ### Fixed
 
+- BUG: Fix hard-coded radius value for parachute added mass calculation [#889](https://github.com/RocketPy-Team/RocketPy/pull/889)
 - BUG: Fix parallel Monte Carlo simulation showing incorrect iteration count [#806](https://github.com/RocketPy-Team/RocketPy/pull/806)
 - BUG: Fix CSV column header spacing in FlightDataExporter [#864](https://github.com/RocketPy-Team/RocketPy/issues/864)
 
diff --git a/rocketpy/rocket/parachute.py b/rocketpy/rocket/parachute.py
index f0bf86f67..90645c4fd 100644
--- a/rocketpy/rocket/parachute.py
+++ b/rocketpy/rocket/parachute.py
@@ -94,8 +94,9 @@ class Parachute:
         Function of clean_pressure_signal.
     Parachute.radius : float
         Length of the non-unique semi-axis (radius) of the inflated hemispheroid
-        parachute in meters.
-    Parachute.height : float, None
+        parachute in meters. Estimated from ``cd_s`` using the formula
+        ``R = sqrt(cd_s / (1.4 * π))`` if not explicitly provided.
+    Parachute.height : float
         Length of the unique semi-axis (height) of the inflated hemispheroid
         parachute in meters.
     Parachute.porosity : float
@@ -108,6 +109,10 @@ class Parachute:
         calculated from the porosity of the parachute.
     """
 
+    # Typical drag coefficient for hemispherical parachute
+    # Used to estimate radius from cd_s when radius is not provided
+    HEMISPHERICAL_CD = 1.4
+
     def __init__(
         self,
         name,
@@ -116,7 +121,7 @@ def __init__(
         sampling_rate,
         lag=0,
         noise=(0, 0, 0),
-        radius=1.5,
+        radius=None,
         height=None,
         porosity=0.0432,
     ):
@@ -173,7 +178,9 @@ def __init__(
             Units are in Pa.
         radius : float, optional
             Length of the non-unique semi-axis (radius) of the inflated hemispheroid
-            parachute. Default value is 1.5.
+            parachute. If not provided, it is estimated from ``cd_s`` assuming a
+            typical hemispherical parachute drag coefficient of 1.4, using the
+            formula: ``radius = sqrt(cd_s / (HEMISPHERICAL_CD * pi))``.
             Units are in meters.
         height : float, optional
             Length of the unique semi-axis (height) of the inflated hemispheroid
@@ -200,8 +207,13 @@ def __init__(
         self.clean_pressure_signal_function = Function(0)
         self.noisy_pressure_signal_function = Function(0)
         self.noise_signal_function = Function(0)
-        self.radius = radius
-        self.height = height or radius
+        # Estimate radius from cd_s if not provided
+        if radius is None:
+            # cd_s = Cd * S = Cd * π * R² => R = sqrt(cd_s / (Cd * π))
+            self.radius = np.sqrt(cd_s / (self.HEMISPHERICAL_CD * np.pi))
+        else:
+            self.radius = radius
+        self.height = height or self.radius
         self.porosity = porosity
         self.added_mass_coefficient = 1.068 * (
             1
@@ -340,7 +352,7 @@ def from_dict(cls, data):
             sampling_rate=data["sampling_rate"],
             lag=data["lag"],
             noise=data["noise"],
-            radius=data.get("radius", 1.5),
+            radius=data.get("radius", None),
             height=data.get("height", None),
             porosity=data.get("porosity", 0.0432),
         )