diff --git a/rocketpy/simulation/flight.py b/rocketpy/simulation/flight.py
index 55ca3486f..cc804d0e1 100644
--- a/rocketpy/simulation/flight.py
+++ b/rocketpy/simulation/flight.py
@@ -1225,6 +1225,8 @@ def __handle_impact_event(self, phase, phase_index, node_index):
         ]
         if len(valid_t_root) > 1:  # pragma: no cover
             raise ValueError("Multiple roots found when solving for impact time.")
+        if len(valid_t_root) == 0:
+            raise ValueError("No valid roots found when solving for impact time.")
         # Determine impact state at t_root
         self.t = self.t_final = valid_t_root[0] + self.solution[-2][0]
         interpolator = phase.solver.dense_output()
diff --git a/tests/unit/simulation/test_flight.py b/tests/unit/simulation/test_flight.py
index 9a3c54477..391d89411 100644
--- a/tests/unit/simulation/test_flight.py
+++ b/tests/unit/simulation/test_flight.py
@@ -1,6 +1,7 @@
 import json
 import os
-from unittest.mock import patch
+from types import SimpleNamespace
+from unittest.mock import MagicMock, patch
 
 import matplotlib as plt
 import numpy as np
@@ -84,6 +85,65 @@ def compute_static_margin_error_given_distance(position, static_margin, rocket):
 # Tests
 
 
+def _make_impact_event_state():
+    flight = object.__new__(Flight)
+    flight.env = SimpleNamespace(elevation=0)
+    flight.solution = [
+        [10.0, 0, 0, 1, 0, 0, -1],
+        [11.0, 0, 0, -1, 0, 0, -1],
+    ]
+    flight.flight_phases = SimpleNamespace(
+        flush_after=MagicMock(), add_phase=MagicMock()
+    )
+
+    solver = SimpleNamespace(
+        step_size=1.0,
+        dense_output=lambda: lambda _: np.array([2, 3, 0, 4, 5, -6]),
+        status="running",
+    )
+    time_nodes = SimpleNamespace(flush_after=MagicMock(), add_node=MagicMock())
+    phase = SimpleNamespace(solver=solver, time_nodes=time_nodes)
+    return flight, phase
+
+
+@pytest.mark.parametrize(
+    "roots, match",
+    [
+        ([-1 + 0j, 2 + 0j], "No valid roots found"),
+        ([0.25 + 0j, 0.75 + 0j], "Multiple roots found"),
+    ],
+)
+def test_handle_impact_event_reports_invalid_root_counts(roots, match):
+    flight, phase = _make_impact_event_state()
+
+    with patch(
+        "rocketpy.simulation.flight.find_roots_cubic_function", return_value=roots
+    ):
+        with pytest.raises(ValueError, match=match):
+            flight._Flight__handle_impact_event(phase, phase_index=1, node_index=2)
+
+
+def test_handle_impact_event_uses_single_valid_root():
+    flight, phase = _make_impact_event_state()
+
+    with patch(
+        "rocketpy.simulation.flight.find_roots_cubic_function",
+        return_value=[0.5 + 0j],
+    ):
+        handled = flight._Flight__handle_impact_event(
+            phase, phase_index=1, node_index=2
+        )
+
+    assert handled is True
+    assert flight.t == flight.t_final == pytest.approx(10.5)
+    assert flight.impact_velocity == -6
+    assert phase.solver.status == "finished"
+    flight.flight_phases.flush_after.assert_called_once_with(1)
+    flight.flight_phases.add_phase.assert_called_once_with(10.5)
+    phase.time_nodes.flush_after.assert_called_once_with(2)
+    phase.time_nodes.add_node.assert_called_once_with(10.5, [], [], [])
+
+
 def test_get_solution_at_time(flight_calisto):
     """Test the get_solution_at_time method of the Flight class. This test
     simply calls the method at the initial and final time and checks if the