diff --git a/.github/workflows/test-pytest.yaml b/.github/workflows/test-pytest.yaml
index 68855c2..c73dd21 100644
--- a/.github/workflows/test-pytest.yaml
+++ b/.github/workflows/test-pytest.yaml
@@ -15,7 +15,7 @@ jobs:
     strategy:
       matrix:
         os: [ubuntu-latest, windows-latest]
-        python-version: [3.8, 3.12]
+        python-version: [3.9, 3.12]
     env:
       OS: ${{ matrix.os }}
       PYTHON: ${{ matrix.python-version }}
diff --git a/Makefile b/Makefile
new file mode 100644
index 0000000..4a6e122
--- /dev/null
+++ b/Makefile
@@ -0,0 +1,20 @@
+lint: isort black
+
+isort:
+	isort .
+
+black:
+	black .
+
+pylint:
+	pylint rocketserializer/ --output="pylint_report.txt"
+
+tests:
+	pytest
+
+# tests-unit:
+
+# tests-acceptance:
+
+# tests-integration:
+
diff --git a/examples/EPFL--BellaLui--2020/parameters.json b/examples/EPFL--BellaLui--2020/parameters.json
index 90f819a..581e7a9 100644
--- a/examples/EPFL--BellaLui--2020/parameters.json
+++ b/examples/EPFL--BellaLui--2020/parameters.json
@@ -42,7 +42,7 @@
         "nozzle_radius": 0.02025,
         "position": 2.3379117844381234,
         "throat_radius": 0.0135,
-        "thrust_source": "examples/EPFL--BellaLui--2020/thrust_source.csv"
+        "thrust_source": "examples\\EPFL--BellaLui--2020\\thrust_source.csv"
     },
     "nosecones": {
         "base_radius": 0.078,
@@ -56,7 +56,7 @@
     "rocket": {
         "center_of_mass_without_propellant": 1.559,
         "coordinate_system_orientation": "nose_to_tail",
-        "drag_curve": "examples/EPFL--BellaLui--2020/drag_curve.csv",
+        "drag_curve": "examples\\EPFL--BellaLui--2020\\drag_curve.csv",
         "inertia": [
             0.096246,
             0.096246,
@@ -66,13 +66,17 @@
         "radius": 0.078
     },
     "stored_results": {
+        "burnout_stability_margin": 3.1703,
         "flight_time": 92.782,
         "ground_hit_velocity": 26.142,
         "launch_rod_velocity": 14.728,
         "max_acceleration": 122.07,
         "max_altitude": 1190.0,
         "max_mach": 0.5587,
+        "max_stability_margin": 4.8193,
+        "max_thrust": 1287.5,
         "max_velocity": 189.56,
+        "min_stability_margin": 0.85185,
         "time_to_apogee": 14.851
     },
     "tails": {
diff --git a/examples/NDRT--Rocket--2020/parameters.json b/examples/NDRT--Rocket--2020/parameters.json
index 2d34c2b..0a3e057 100644
--- a/examples/NDRT--Rocket--2020/parameters.json
+++ b/examples/NDRT--Rocket--2020/parameters.json
@@ -1,4 +1,5 @@
 {
+    "elliptical_fins": {},
     "environment": {
         "base_pressure": null,
         "base_temperature": null,
@@ -84,13 +85,17 @@
         "radius": 0.1016
     },
     "stored_results": {
+        "burnout_stability_margin": 3.7288,
         "flight_time": 86.725,
         "ground_hit_velocity": 4.7426,
         "launch_rod_velocity": 17.993,
         "max_acceleration": 67.386,
         "max_altitude": 1085.9,
         "max_mach": 0.42789,
+        "max_stability_margin": 3.7685,
+        "max_thrust": 1785.0,
         "max_velocity": 145.01,
+        "min_stability_margin": 1.2489,
         "time_to_apogee": 15.761
     },
     "tails": {
diff --git a/examples/ProjetoJupiter--Valetudo--2019/parameters.json b/examples/ProjetoJupiter--Valetudo--2019/parameters.json
index 84168b8..f57c4e6 100644
--- a/examples/ProjetoJupiter--Valetudo--2019/parameters.json
+++ b/examples/ProjetoJupiter--Valetudo--2019/parameters.json
@@ -1,4 +1,5 @@
 {
+    "elliptical_fins": {},
     "environment": {
         "base_pressure": 94311.0,
         "base_temperature": 300.76,
@@ -81,13 +82,17 @@
         "radius": 0.04045000000000001
     },
     "stored_results": {
+        "burnout_stability_margin": 2.4363,
         "flight_time": 64.161,
         "ground_hit_velocity": 18.146,
         "launch_rod_velocity": 26.397,
         "max_acceleration": 108.52,
         "max_altitude": 882.42,
         "max_mach": 0.36177,
+        "max_stability_margin": 3.2714,
+        "max_thrust": 1067.7,
         "max_velocity": 125.47,
+        "min_stability_margin": 0.0,
         "time_to_apogee": 14.65
     },
     "tails": {},
diff --git a/pyproject.toml b/pyproject.toml
index 1525d05..4a777d8 100644
--- a/pyproject.toml
+++ b/pyproject.toml
@@ -76,4 +76,5 @@ disable = """
     raise-missing-from,
     fixme,
     no-else-break,
+    no-else-return,
 """
diff --git a/rocketserializer/components/stored_results.py b/rocketserializer/components/stored_results.py
index ab762a7..d4cd511 100644
--- a/rocketserializer/components/stored_results.py
+++ b/rocketserializer/components/stored_results.py
@@ -1,11 +1,13 @@
 import logging
 
+import numpy as np
+
 from .._helpers import _dict_to_string
 
 logger = logging.getLogger(__name__)
 
 
-def search_stored_results(bs):
+def search_stored_results(bs, datapoints, data_labels, time_vector, burnout_position):
     """Search for the stored simulation results in the bs and return the
     settings as a dict.
 
@@ -22,11 +24,9 @@ def search_stored_results(bs):
         "flighttime", "groundhitvelocity" and "launchrodvelocity".
     """
     settings = {}
-
     sim = bs.find("simulation")
     sim_data = sim.find("flightdata")
     logger.info("Found the 'flightdata' tag in the 'simulation' tag.")
-
     name_map = {
         "max_altitude": "maxaltitude",
         "max_velocity": "maxvelocity",
@@ -44,8 +44,84 @@ def search_stored_results(bs):
             "Retrieved the '%s' value from the .ork file: %s", key, settings[key]
         )
 
+    settings["max_stability_margin"] = __get_parameter(
+        datapoints,
+        data_labels,
+        time_vector,
+        "Stability margin calibers",
+        position="max",
+    )
+    settings["min_stability_margin"] = __get_parameter(
+        datapoints,
+        data_labels,
+        time_vector,
+        "Stability margin calibers",
+        position="min",
+    )
+    settings["burnout_stability_margin"] = __get_parameter(
+        datapoints,
+        data_labels,
+        time_vector,
+        "Stability margin calibers",
+        position=burnout_position,
+    )
+    settings["max_thrust"] = __get_parameter(
+        datapoints, data_labels, time_vector, "Thrust", position="max"
+    )
+
     logger.info(
         "The flight data was successfully retrieved:\n%s",
         _dict_to_string(settings, indent=23),
     )
     return settings
+
+
+def __get_parameter(datapoints, data_labels, time_vector, label, position):
+    """Get the latitude and longitude from the .ork file.
+    Parameters
+    ----------
+    label : str
+        Latitude or longitude.
+    datapoints : list
+        List of datapoints from the .ork file.
+    data_labels : list
+        List of labels for the datapoints.
+    time_vector : list
+        The time vector of the simulation.
+    position : str or int
+        The position to get the value from. Can be "last", "first", "max", "min"
+        or an integer.
+    """
+
+    parameter = [
+        float(datapoint.text.split(",")[data_labels.index(label)])
+        for datapoint in datapoints
+    ]
+    # convert to numpy array
+    parameter = np.array([time_vector, parameter]).T
+    # sort by time
+    parameter = parameter[parameter[:, 0].argsort()]
+    # clip the curve to remove negative values
+    parameter[parameter[:, 1] < 0, 1] = 0
+    # Assuming parameter is a NumPy array and 'NaN' values are represented as np.nan
+    # This will keep rows where the second column is not NaN
+    parameter = parameter[~np.isnan(parameter[:, 1])]
+
+    if isinstance(position, str):
+        if position == "last":
+            # return the end point (final time, final value)
+            return parameter[-1, 1]
+        elif position == "first":
+            # return the first point (initial time, initial value)
+            return parameter[0, 1]
+        elif position == "max":
+            return np.max(parameter[:, 1])  # return the maximum value
+        elif position == "min":
+            return np.min(parameter[:, 1])  # return the minimum value
+    else:
+        pass
+    if isinstance(position, np.int64):
+        return parameter[position, 1]  # return the value at the specified position
+    else:
+        logger.error("Invalid position parameter")
+        raise ValueError("Error in position parameter")
diff --git a/rocketserializer/ork_extractor.py b/rocketserializer/ork_extractor.py
index 8abd39a..fc5280c 100644
--- a/rocketserializer/ork_extractor.py
+++ b/rocketserializer/ork_extractor.py
@@ -88,7 +88,9 @@ def ork_extractor(bs, filepath, output_folder, ork, eng):
     transitions = search_transitions(bs, elements, ork)
     rail_buttons = search_rail_buttons(bs, elements)
     parachutes = search_parachutes(bs)
-    stored_results = search_stored_results(bs)
+    stored_results = search_stored_results(
+        bs, datapoints, data_labels, time_vector, burnout_position
+    )
 
     # save everything to a dictionary
     settings["id"] = id_info
diff --git a/run-tests.ps1 b/run-tests.ps1
index cf2bc43..416eb7c 100644
--- a/run-tests.ps1
+++ b/run-tests.ps1
@@ -1,3 +1,9 @@
 ork2json --filepath="examples\EPFL--BellaLui--2020\rocket.ork"
 ork2json --filepath="examples\NDRT--Rocket--2020\rocket.ork"
 ork2json --filepath="examples\ProjetoJupiter--Valetudo--2019\rocket.ork"
+ork2json --filepath="examples\WERT--Prometheus--2022\rocket.ork"
+
+ork2ipynb --filepath="examples\EPFL--BellaLui--2020\rocket.ork"
+ork2ipynb --filepath="examples\NDRT--Rocket--2020\rocket.ork"
+ork2ipynb --filepath="examples\ProjetoJupiter--Valetudo--2019\rocket.ork"
+ork2ipynb --filepath="examples\WERT--Prometheus--2022\rocket.ork"
diff --git a/tests/acceptance/EPFL--BellaLui--2020/parameters.json b/tests/acceptance/EPFL--BellaLui--2020/parameters.json
index fc7f04e..4c1151e 100644
--- a/tests/acceptance/EPFL--BellaLui--2020/parameters.json
+++ b/tests/acceptance/EPFL--BellaLui--2020/parameters.json
@@ -96,6 +96,10 @@
         "time_to_apogee": 14.851,
         "flight_time": 92.782,
         "ground_hit_velocity": 26.142,
-        "launch_rod_velocity": 14.728
+        "launch_rod_velocity": 14.728,
+        "max_stability_margin": 4.8193,
+        "min_stability_margin": 0.85185,
+        "burnout_stability_margin": 3.1703,
+        "max_thrust": 1287.5
     }
 }
\ No newline at end of file
diff --git a/tests/acceptance/NDRT--Rocket--2020/parameters.json b/tests/acceptance/NDRT--Rocket--2020/parameters.json
index 23616b8..5105b69 100644
--- a/tests/acceptance/NDRT--Rocket--2020/parameters.json
+++ b/tests/acceptance/NDRT--Rocket--2020/parameters.json
@@ -115,6 +115,10 @@
         "time_to_apogee": 15.761,
         "flight_time": 86.725,
         "ground_hit_velocity": 4.7426,
-        "launch_rod_velocity": 17.993
+        "launch_rod_velocity": 17.993,
+        "max_stability_margin": 3.7685,
+        "min_stability_margin": 1.2489,
+        "burnout_stability_margin": 3.7288,
+        "max_thrust": 1785.0
     }
 }
\ No newline at end of file
diff --git a/tests/acceptance/ProjetoJupiter--Valetudo--2019/parameters.json b/tests/acceptance/ProjetoJupiter--Valetudo--2019/parameters.json
index e410b2b..a282666 100644
--- a/tests/acceptance/ProjetoJupiter--Valetudo--2019/parameters.json
+++ b/tests/acceptance/ProjetoJupiter--Valetudo--2019/parameters.json
@@ -104,6 +104,10 @@
         "time_to_apogee": 14.65,
         "flight_time": 64.161,
         "ground_hit_velocity": 18.146,
-        "launch_rod_velocity": 26.397
+        "launch_rod_velocity": 26.397,
+        "max_stability_margin": 3.2714,
+        "min_stability_margin": 0.0,
+        "burnout_stability_margin": 2.4363,
+        "max_thrust": 1067.7
     }
 }
\ No newline at end of file