mnt: applying review suggestions

Lucas-Prates · Lucas-Prates · commit 5bfc866e6925 · 2026-05-07T23:00:01.000-03:00
diff --git a/docs/examples/andromeda_flight_sim.ipynb b/docs/examples/andromeda_flight_sim.ipynb
@@ -290,8 +290,8 @@
     "Main = HemisphericalParachute(\n",
     "    \"Main\", cd_s=8.362919643856031, trigger=500, sampling_rate=100, lag=0\n",
     ")\n",
-    "Andromeda.add_parachute(parachute = Drogue)\n",
-    "Andromeda.add_parachute(parachute = Main)"
+    "Andromeda.add_parachute(parachute=Drogue)\n",
+    "Andromeda.add_parachute(parachute=Main)"
    ]
   },
   {
diff --git a/docs/examples/bella_lui_flight_sim.ipynb b/docs/examples/bella_lui_flight_sim.ipynb
@@ -441,7 +441,7 @@
     "    lag=parameters.get(\"lag_rec\")[0],\n",
     "    noise=(0, 8.3, 0.5),\n",
     ")\n",
-    "bella_lui.add_parachute(parachute = Drogue)"
+    "bella_lui.add_parachute(parachute=Drogue)"
    ]
   },
   {
diff --git a/docs/examples/camoes_flight_sim.ipynb b/docs/examples/camoes_flight_sim.ipynb
@@ -311,7 +311,7 @@
     "Drogue = HemisphericalParachute(\n",
     "    \"Drogue\", cd_s=0.33, sampling_rate=400, lag=1.5, trigger=drogue_trigger\n",
     ")\n",
-    "CAMOES.add_parachute(parachute = Drogue)"
+    "CAMOES.add_parachute(parachute=Drogue)"
    ]
   },
   {
diff --git a/docs/examples/defiance_flight_sim.ipynb b/docs/examples/defiance_flight_sim.ipynb
@@ -228,8 +228,8 @@
     "Drogue = HemisphericalParachute(\n",
     "    name=\"drogue\", cd_s=1.55, trigger=\"apogee\", sampling_rate=100, lag=0\n",
     ")\n",
-    "defiance.add_parachute(parachute = Main)\n",
-    "defiance.add_parachute(parachute = Drogue)"
+    "defiance.add_parachute(parachute=Main)\n",
+    "defiance.add_parachute(parachute=Drogue)"
    ]
   },
   {
diff --git a/docs/examples/genesis_flight_sim.ipynb b/docs/examples/genesis_flight_sim.ipynb
@@ -288,8 +288,8 @@
     "    lag=1,\n",
     "    noise=(0, 8.3, 0.5),\n",
     ")\n",
-    "GENESIS.add_parachute(parachute = Drogue)\n",
-    "GENESIS.add_parachute(parachute = Main)"
+    "GENESIS.add_parachute(parachute=Drogue)\n",
+    "GENESIS.add_parachute(parachute=Main)"
    ]
   },
   {
diff --git a/docs/examples/halcyon_flight_sim.ipynb b/docs/examples/halcyon_flight_sim.ipynb
@@ -427,7 +427,7 @@
     "    sampling_rate=100,\n",
     "    lag=5,\n",
     ")\n",
-    "HALCYON.add_parachute(parachute = Main)"
+    "HALCYON.add_parachute(parachute=Main)"
    ]
   },
   {
diff --git a/docs/examples/juno3_flight_sim.ipynb b/docs/examples/juno3_flight_sim.ipynb
@@ -352,7 +352,7 @@
     "    noise=(0, 8.3, 0.5),\n",
     "    lag=0.5,\n",
     ")\n",
-    "juno.add_parachute(parachute = drogue)"
+    "juno.add_parachute(parachute=drogue)"
    ]
   },
   {
diff --git a/docs/examples/lince_flight_sim.ipynb b/docs/examples/lince_flight_sim.ipynb
@@ -272,7 +272,7 @@
     "Main = HemisphericalParachute(\n",
     "    \"Main\", cd_s=3.9, trigger=\"apogee\", sampling_rate=150, lag=0, noise=(0, 0, 0)\n",
     ")\n",
-    "LincePreDeploy.add_parachute(parachute = Main)"
+    "LincePreDeploy.add_parachute(parachute=Main)"
    ]
   },
   {
@@ -336,7 +336,7 @@
     "Main_stage_1 = HemisphericalParachute(\n",
     "    \"Main\", cd_s=3.9, trigger=\"apogee\", sampling_rate=150, lag=0, noise=(0, 0, 0)\n",
     ")\n",
-    "LincePostDeploy.add_parachute(parachute = Main_stage_1)"
+    "LincePostDeploy.add_parachute(parachute=Main_stage_1)"
    ]
   },
   {
@@ -405,7 +405,7 @@
     "Main_stage_2 = HemisphericalParachute(\n",
     "    \"Main\", cd_s=0.159248, trigger=\"apogee\", sampling_rate=150, lag=0, noise=(0, 0, 0)\n",
     ")\n",
-    "Payload.add_parachute(parachute = Main_stage_2)"
+    "Payload.add_parachute(parachute=Main_stage_2)"
    ]
   },
   {
diff --git a/docs/examples/ndrt_2020_flight_sim.ipynb b/docs/examples/ndrt_2020_flight_sim.ipynb
@@ -395,8 +395,8 @@
     "    noise=(0, 8.3, 0.5),\n",
     ")\n",
     "\n",
-    "ndrt2020.add_parachute(parachute = drogue)\n",
-    "ndrt2020.add_parachute(parachute = main)"
+    "ndrt2020.add_parachute(parachute=drogue)\n",
+    "ndrt2020.add_parachute(parachute=main)"
    ]
   },
   {
diff --git a/docs/examples/prometheus_2022_flight_sim.ipynb b/docs/examples/prometheus_2022_flight_sim.ipynb
@@ -293,8 +293,8 @@
     "    trigger=457.2,  # 1500 ft\n",
     ")\n",
     "\n",
-    "prometheus.add_parachute(parachute = drogue)\n",
-    "prometheus.add_parachute(parachute = main)"
+    "prometheus.add_parachute(parachute=drogue)\n",
+    "prometheus.add_parachute(parachute=main)"
    ]
   },
   {
diff --git a/docs/examples/valetudo_flight_sim.ipynb b/docs/examples/valetudo_flight_sim.ipynb
@@ -395,7 +395,7 @@
     "    lag=parameters.get(\"lag_rec\")[0],\n",
     "    noise=(0, 8.3, 0.5),\n",
     ")\n",
-    "valetudo.add_parachute(parachute = drogue)"
+    "valetudo.add_parachute(parachute=drogue)"
    ]
   },
   {
diff --git a/docs/notebooks/getting_started.ipynb b/docs/notebooks/getting_started.ipynb
@@ -747,8 +747,8 @@
     "    noise=(0, 8.3, 0.5),\n",
     ")\n",
     "\n",
-    "calisto.add_parachute(parachute = Main)\n",
-    "calisto.add_parachute(parachute = Drogue)"
+    "calisto.add_parachute(parachute=Main)\n",
+    "calisto.add_parachute(parachute=Drogue)"
    ]
   },
   {
diff --git a/docs/notebooks/getting_started_colab.ipynb b/docs/notebooks/getting_started_colab.ipynb
@@ -503,8 +503,8 @@
     "    noise=(0, 8.3, 0.5),\n",
     ")\n",
     "\n",
-    "calisto.add_parachute(parachute = Main)\n",
-    "calisto.add_parachute(parachute = Drogue)"
+    "calisto.add_parachute(parachute=Main)\n",
+    "calisto.add_parachute(parachute=Drogue)"
    ]
   },
   {
diff --git a/docs/notebooks/monte_carlo_analysis/monte_carlo_class_usage.ipynb b/docs/notebooks/monte_carlo_analysis/monte_carlo_class_usage.ipynb
@@ -622,8 +622,8 @@
     "stochastic_rocket.set_rail_buttons(\n",
     "    stochastic_rail_buttons, lower_button_position=(0.001, \"normal\")\n",
     ")\n",
-    "stochastic_rocket.add_parachute(parachute = stochastic_main)\n",
-    "stochastic_rocket.add_parachute(parachute = stochastic_drogue)"
+    "stochastic_rocket.add_parachute(parachute=stochastic_main)\n",
+    "stochastic_rocket.add_parachute(parachute=stochastic_drogue)"
    ]
   },
   {
diff --git a/rocketpy/__init__.py b/rocketpy/__init__.py
@@ -39,6 +39,7 @@
     HemisphericalParachute,
     LinearGenericSurface,
     NoseCone,
+    Parachute,
     PointMassRocket,
     RailButtons,
     Rocket,
diff --git a/rocketpy/rocket/__init__.py b/rocketpy/rocket/__init__.py
@@ -17,6 +17,6 @@
     TrapezoidalFins,
 )
 from rocketpy.rocket.components import Components
-from rocketpy.rocket.parachutes import HemisphericalParachute
+from rocketpy.rocket.parachutes import HemisphericalParachute, Parachute
 from rocketpy.rocket.point_mass_rocket import PointMassRocket
 from rocketpy.rocket.rocket import Rocket
diff --git a/rocketpy/rocket/parachutes/__init__.py b/rocketpy/rocket/parachutes/__init__.py
@@ -1 +1,2 @@
 from .hemispherical_parachute import HemisphericalParachute
+from .parachute import Parachute
diff --git a/rocketpy/rocket/parachutes/hemispherical_parachute.py b/rocketpy/rocket/parachutes/hemispherical_parachute.py
@@ -3,10 +3,10 @@
 from rocketpy.tools import from_hex_decode, to_hex_encode
 
 from ...mathutils.function import Function
-from .base_parachute import BaseParachute
+from .parachute import Parachute
 
 
-class HemisphericalParachute(BaseParachute):
+class HemisphericalParachute(Parachute):
     """Implements a hemispherical parachute.
 
     Attributes
@@ -24,7 +24,7 @@ class HemisphericalParachute(BaseParachute):
         This parameter defines the trigger condition for the parachute ejection
         system. It can be one of the following:
 
-        - A callable function that takes three arguments:
+        - A callable function that takes four arguments:
           1. Freestream pressure in pascals.
           2. Height in meters above ground level.
           3. The state vector of the simulation, which is defined as:
@@ -289,9 +289,13 @@ def u_dot(self, t, u, flight_information, post_processing=False):
 
         Return
         ------
-        u_dot : list
-            State vector defined by u_dot = [vx, vy, vz, ax, ay, az,
-            e0dot, e1dot, e2dot, e3dot, alpha1, alpha2, alpha3].
+        u_dot : dict
+            A dictionary containing two or three keys
+            1) state: State vector which depends on the parachute model.
+            2) additional_information: information as dict that is added
+            to the  'parachutes_info' attribute in the Flight class.
+            3) post_processing_information: State vector containing
+            post processing information.
 
         """
         # Get relevant state data
@@ -308,15 +312,6 @@ def u_dot(self, t, u, flight_information, post_processing=False):
         # Get the mass of the rocket
         mp = rocket.dry_mass
 
-        # to = 1.2
-        # eta = 1
-        # Rdot = (6 * R * (1 - eta) / (1.2**6)) * (
-        #     (1 - eta) * t**5 + eta * (to**3) * (t**2)
-        # )
-        # Rdot = 0
-
-        # tf = 8 * nominal diameter / velocity at line stretch
-
         # Calculate added mass
         ma = (
             self.added_mass_coefficient
@@ -335,8 +330,7 @@ def u_dot(self, t, u, flight_information, post_processing=False):
 
         # Determine drag force
         pseudo_drag = -0.5 * rho * self.cd_s * free_stream_speed
-        # pseudo_drag = pseudo_drag - ka * rho * 4 * np.pi * (R**2) * Rdot
-        Dx = pseudo_drag * freestream_x  # add eta efficiency for wake
+        Dx = pseudo_drag * freestream_x
         Dy = pseudo_drag * freestream_y
         Dz = pseudo_drag * freestream_z
         total_drag = np.sqrt(Dx**2 + Dy**2 + Dz**2)
@@ -360,26 +354,22 @@ def u_dot(self, t, u, flight_information, post_processing=False):
         }
 
         if post_processing:
-            data_dict = {
-                "state": [vx, vy, vz, ax, ay, az, 0, 0, 0, 0, 0, 0, 0],
-                "post_processing_information": [
-                    t,
-                    ax,
-                    ay,
-                    az,
-                    0,
-                    0,
-                    0,
-                    Dx,
-                    Dy,
-                    Dz,
-                    0,
-                    0,
-                    0,
-                    0,
-                ],
-            }
-            return data_dict
+            output["post_processing_information"] = [
+                t,
+                ax,
+                ay,
+                az,
+                0,
+                0,
+                0,
+                Dx,
+                Dy,
+                Dz,
+                0,
+                0,
+                0,
+                0,
+            ]
         return output
 
     # serialization methods
diff --git a/rocketpy/simulation/flight.py b/rocketpy/simulation/flight.py
@@ -2567,7 +2567,7 @@ def u_dot_parachute_wrapper(self, parachute):
         each parachute implements its own u_dot. This u_dot takes as argument the
         state variable 'u', the time 't', and additional flight information as
         'flight_information'. However, the solver (which is in the Flight class)
-        only allos u_dot to take 'u' and 't' as arguments. Hence, this wrapper
+        only allows u_dot to take 'u' and 't' as arguments. Hence, this wrapper
         wraps the output of the u_dot to match the expected arguments of the
         solver.
 
diff --git a/rocketpy/stochastic/stochastic_rocket.py b/rocketpy/stochastic/stochastic_rocket.py
@@ -17,7 +17,7 @@
     TrapezoidalFins,
 )
 from rocketpy.rocket.components import Components
-from rocketpy.rocket.parachutes import HemisphericalParachute
+from rocketpy.rocket.parachutes.parachute import Parachute
 from rocketpy.rocket.rocket import Rocket
 from rocketpy.stochastic.stochastic_generic_motor import StochasticGenericMotor
 from rocketpy.stochastic.stochastic_motor_model import StochasticMotorModel
@@ -360,11 +360,11 @@ def add_parachute(self, parachute):
             The parachute to be added to the stochastic rocket.
         """
         # checks if input is a StochasticParachute type
-        if not isinstance(parachute, (HemisphericalParachute, StochasticParachute)):
+        if not isinstance(parachute, (Parachute, StochasticParachute)):
             raise TypeError(
-                "`parachute` must be of Parachute or StochasticParachute type"
+                "`parachute` must be of valid parachute model or StochasticParachute type"
             )
-        if isinstance(parachute, HemisphericalParachute):
+        if isinstance(parachute, Parachute):
             parachute = StochasticParachute(parachute=parachute)
         self.parachutes.append(parachute)
 
@@ -795,6 +795,6 @@ def create_object(self):
 
         for parachute in self.parachutes:
             parachute = self._create_parachute(parachute)
-            rocket.add_parachute(parachute = parachute)
+            rocket.add_parachute(parachute=parachute)
 
         return rocket
diff --git a/tests/acceptance/test_bella_lui_rocket.py b/tests/acceptance/test_bella_lui_rocket.py
@@ -146,7 +146,7 @@ def drogue_trigger(p, h, y):
         lag=parameters.get("lag_rec")[0],
         noise=(0, 8.3, 0.5),
     )
-    BellaLui.add_parachute(parachute = drogue)
+    BellaLui.add_parachute(parachute=drogue)
 
     # Define aerodynamic drag coefficients
     power_off_drag_by_mach = Function(
diff --git a/tests/acceptance/test_ndrt_2020_rocket.py b/tests/acceptance/test_ndrt_2020_rocket.py
@@ -170,8 +170,8 @@ def main_trigger(p, h, y):  # pylint: disable=unused-argument
         lag=parameters.get("lag_rec")[0],
         noise=(0, 8.3, 0.5),
     )
-    NDRT2020.add_parachute(parachute = drogue)
-    NDRT2020.add_parachute(parachute = main)
+    NDRT2020.add_parachute(parachute=drogue)
+    NDRT2020.add_parachute(parachute=main)
 
     # Flight
     rocketpy_flight = Flight(
diff --git a/tests/fixtures/monte_carlo/stochastic_fixtures.py b/tests/fixtures/monte_carlo/stochastic_fixtures.py
@@ -240,8 +240,8 @@ def stochastic_calisto(
     rocket.set_rail_buttons(
         stochastic_rail_buttons, lower_button_position=(-0.618, 0.001, "normal")
     )
-    rocket.add_parachute(parachute = stochastic_main_parachute)
-    rocket.add_parachute(parachute = stochastic_drogue_parachute)
+    rocket.add_parachute(parachute=stochastic_main_parachute)
+    rocket.add_parachute(parachute=stochastic_drogue_parachute)
     return rocket
 
 
diff --git a/tests/fixtures/rockets/rocket_fixtures.py b/tests/fixtures/rockets/rocket_fixtures.py
@@ -416,6 +416,6 @@ def prometheus_cd_at_ma(mach):
         trigger=457.2,  # 1500 ft
         sampling_rate=100,
     )
-    prometheus.add_parachute(parachute = drogue)
-    prometheus.add_parachute(parachute = main)
+    prometheus.add_parachute(parachute=drogue)
+    prometheus.add_parachute(parachute=main)
     return prometheus
diff --git a/tests/integration/simulation/test_flight.py b/tests/integration/simulation/test_flight.py
@@ -172,9 +172,9 @@ def test_simpler_parachute_triggers(mock_show, example_plain_env, calisto_robust
         sampling_rate=105,
         lag=0,
     )
-    calisto_robust.add_parachute(parachute = main)
-    calisto_robust.add_parachute(parachute = drogue1)
-    calisto_robust.add_parachute(parachute = drogue2)
+    calisto_robust.add_parachute(parachute=main)
+    calisto_robust.add_parachute(parachute=drogue1)
+    calisto_robust.add_parachute(parachute=drogue2)
 
     test_flight = Flight(
         rocket=calisto_robust,
@@ -205,7 +205,7 @@ def test_simpler_parachute_triggers(mock_show, example_plain_env, calisto_robust
     assert test_flight.all_info() is None
 
 
-#TODO: When the legacy behavior is removed, remove this test
+# TODO: When the legacy behavior is removed, remove this test
 @patch("matplotlib.pyplot.show")
 def test_legacy_add_parachute(mock_show, example_plain_env, calisto_robust):  # pylint: disable=unused-argument
     """This is a legacy test that repeats the tests in 'test_simpler_parachute_triggers'

Original file line number	Diff line number	Diff line change
`@@ -290,8 +290,8 @@`
`290`	`290`	`"Main = HemisphericalParachute(\n",`
`291`	`291`	`" \"Main\", cd_s=8.362919643856031, trigger=500, sampling_rate=100, lag=0\n",`
`292`	`292`	`")\n",`
`293`		`- "Andromeda.add_parachute(parachute = Drogue)\n",`
`294`		`- "Andromeda.add_parachute(parachute = Main)"`
	`293`	`+ "Andromeda.add_parachute(parachute=Drogue)\n",`
	`294`	`+ "Andromeda.add_parachute(parachute=Main)"`
`295`	`295`	`]`
`296`	`296`	`},`
`297`	`297`	`{`
Original file line number	Diff line number	Diff line change
`@@ -441,7 +441,7 @@`
`441`	`441`	`" lag=parameters.get(\"lag_rec\")[0],\n",`
`442`	`442`	`" noise=(0, 8.3, 0.5),\n",`
`443`	`443`	`")\n",`
`444`		`- "bella_lui.add_parachute(parachute = Drogue)"`
	`444`	`+ "bella_lui.add_parachute(parachute=Drogue)"`
`445`	`445`	`]`
`446`	`446`	`},`
`447`	`447`	`{`
Original file line number	Diff line number	Diff line change
`@@ -311,7 +311,7 @@`
`311`	`311`	`"Drogue = HemisphericalParachute(\n",`
`312`	`312`	`" \"Drogue\", cd_s=0.33, sampling_rate=400, lag=1.5, trigger=drogue_trigger\n",`
`313`	`313`	`")\n",`
`314`		`- "CAMOES.add_parachute(parachute = Drogue)"`
	`314`	`+ "CAMOES.add_parachute(parachute=Drogue)"`
`315`	`315`	`]`
`316`	`316`	`},`
`317`	`317`	`{`
Original file line number	Diff line number	Diff line change
`@@ -228,8 +228,8 @@`
`228`	`228`	`"Drogue = HemisphericalParachute(\n",`
`229`	`229`	`" name=\"drogue\", cd_s=1.55, trigger=\"apogee\", sampling_rate=100, lag=0\n",`
`230`	`230`	`")\n",`
`231`		`- "defiance.add_parachute(parachute = Main)\n",`
`232`		`- "defiance.add_parachute(parachute = Drogue)"`
	`231`	`+ "defiance.add_parachute(parachute=Main)\n",`
	`232`	`+ "defiance.add_parachute(parachute=Drogue)"`
`233`	`233`	`]`
`234`	`234`	`},`
`235`	`235`	`{`
Original file line number	Diff line number	Diff line change
`@@ -288,8 +288,8 @@`
`288`	`288`	`" lag=1,\n",`
`289`	`289`	`" noise=(0, 8.3, 0.5),\n",`
`290`	`290`	`")\n",`
`291`		`- "GENESIS.add_parachute(parachute = Drogue)\n",`
`292`		`- "GENESIS.add_parachute(parachute = Main)"`
	`291`	`+ "GENESIS.add_parachute(parachute=Drogue)\n",`
	`292`	`+ "GENESIS.add_parachute(parachute=Main)"`
`293`	`293`	`]`
`294`	`294`	`},`
`295`	`295`	`{`
Original file line number	Diff line number	Diff line change
`@@ -427,7 +427,7 @@`
`427`	`427`	`" sampling_rate=100,\n",`
`428`	`428`	`" lag=5,\n",`
`429`	`429`	`")\n",`
`430`		`- "HALCYON.add_parachute(parachute = Main)"`
	`430`	`+ "HALCYON.add_parachute(parachute=Main)"`
`431`	`431`	`]`
`432`	`432`	`},`
`433`	`433`	`{`
Original file line number	Diff line number	Diff line change
`@@ -352,7 +352,7 @@`
`352`	`352`	`" noise=(0, 8.3, 0.5),\n",`
`353`	`353`	`" lag=0.5,\n",`
`354`	`354`	`")\n",`
`355`		`- "juno.add_parachute(parachute = drogue)"`
	`355`	`+ "juno.add_parachute(parachute=drogue)"`
`356`	`356`	`]`
`357`	`357`	`},`
`358`	`358`	`{`
Original file line number	Diff line number	Diff line change
`@@ -272,7 +272,7 @@`
`272`	`272`	`"Main = HemisphericalParachute(\n",`
`273`	`273`	`" \"Main\", cd_s=3.9, trigger=\"apogee\", sampling_rate=150, lag=0, noise=(0, 0, 0)\n",`
`274`	`274`	`")\n",`
`275`		`- "LincePreDeploy.add_parachute(parachute = Main)"`
	`275`	`+ "LincePreDeploy.add_parachute(parachute=Main)"`
`276`	`276`	`]`
`277`	`277`	`},`
`278`	`278`	`{`
`@@ -336,7 +336,7 @@`
`336`	`336`	`"Main_stage_1 = HemisphericalParachute(\n",`
`337`	`337`	`" \"Main\", cd_s=3.9, trigger=\"apogee\", sampling_rate=150, lag=0, noise=(0, 0, 0)\n",`
`338`	`338`	`")\n",`
`339`		`- "LincePostDeploy.add_parachute(parachute = Main_stage_1)"`
	`339`	`+ "LincePostDeploy.add_parachute(parachute=Main_stage_1)"`
`340`	`340`	`]`
`341`	`341`	`},`
`342`	`342`	`{`
`@@ -405,7 +405,7 @@`
`405`	`405`	`"Main_stage_2 = HemisphericalParachute(\n",`
`406`	`406`	`" \"Main\", cd_s=0.159248, trigger=\"apogee\", sampling_rate=150, lag=0, noise=(0, 0, 0)\n",`
`407`	`407`	`")\n",`
`408`		`- "Payload.add_parachute(parachute = Main_stage_2)"`
	`408`	`+ "Payload.add_parachute(parachute=Main_stage_2)"`
`409`	`409`	`]`
`410`	`410`	`},`
`411`	`411`	`{`
Original file line number	Diff line number	Diff line change
`@@ -395,8 +395,8 @@`
`395`	`395`	`" noise=(0, 8.3, 0.5),\n",`
`396`	`396`	`")\n",`
`397`	`397`	`"\n",`
`398`		`- "ndrt2020.add_parachute(parachute = drogue)\n",`
`399`		`- "ndrt2020.add_parachute(parachute = main)"`
	`398`	`+ "ndrt2020.add_parachute(parachute=drogue)\n",`
	`399`	`+ "ndrt2020.add_parachute(parachute=main)"`
`400`	`400`	`]`
`401`	`401`	`},`
`402`	`402`	`{`
Original file line number	Diff line number	Diff line change
`@@ -293,8 +293,8 @@`
`293`	`293`	`" trigger=457.2, # 1500 ft\n",`
`294`	`294`	`")\n",`
`295`	`295`	`"\n",`
`296`		`- "prometheus.add_parachute(parachute = drogue)\n",`
`297`		`- "prometheus.add_parachute(parachute = main)"`
	`296`	`+ "prometheus.add_parachute(parachute=drogue)\n",`
	`297`	`+ "prometheus.add_parachute(parachute=main)"`
`298`	`298`	`]`
`299`	`299`	`},`
`300`	`300`	`{`