MNT: Simplify Monte Carlo parallel export structure.

docs/notebooks/monte_carlo_analysis/monte_carlo_analysis_outputs/monte_carlo_class_example.errors.txt

@@ -1 +0,0 @@
-{"elevation": 113, "gravity": "'Function from R1 to R1 : (height (m)) \u2192 (gravity (m/s\u00b2))'", "latitude": 39.3897, "longitude": -8.288964, "wind_velocity_x_factor": 1.0, "wind_velocity_y_factor": 1.0, "datum": "SIRGAS2000", "timezone": "UTC", "ensemble_member": 12, "radius": 0.0635026504073287, "mass": 15.682085969389227, "I_11_without_motor": 6.321, "I_22_without_motor": 6.338988882158036, "I_33_without_motor": 0.03130204348386302, "I_12_without_motor": 0, "I_13_without_motor": 0, "I_23_without_motor": 0, "power_off_drag": "'Function from R1 to R1 : (Mach Number) \u2192 (Drag Coefficient with Power Off)'", "power_on_drag": "'Function from R1 to R1 : (Mach Number) \u2192 (Drag Coefficient with Power On)'", "power_off_drag_factor": 1.0, "power_on_drag_factor": 1.0, "center_of_mass_without_motor": 0.0, "coordinate_system_orientation": "tail_to_nose", "parachutes": [{"cd_s": 9.964579481480238, "trigger": 800, "sampling_rate": 105, "lag": 1.5400928421750208, "noise": [0, 8.3, 0.5], "name": "Main"}, {"cd_s": 1.053581347292585, "trigger": "apogee", "sampling_rate": 105, "lag": 1.547076677223584, "noise": [0, 8.3, 0.5], "name": "Drogue"}], "motors": [{"thrust_source": [[0, 0], [0.055, 100.0], [0.092, 1500.0], [0.1, 2000.0], [0.15, 2200.0], [0.2, 1800.0], [0.5, 1950.0], [1.0, 2034.0], [1.5, 2000.0], [2.0, 1900.0], [2.5, 1760.0], [2.9, 1700.0], [3.0, 1650.0], [3.3, 530.0], [3.4, 350.0], [3.9, 0.0]], "total_impulse": 6856.354770975974, "burn_start_time": 0, "burn_out_time": 3.9, "dry_mass": 1.815, "dry_I_11": 0.125, "dry_I_22": 0.125, "dry_I_33": 0.002, "dry_I_12": 0, "dry_I_13": 0, "dry_I_23": 0, "nozzle_radius": 0.032730650070270366, "grain_number": 5, "grain_density": 1759.0002074492309, "grain_outer_radius": 0.03242230462181787, "grain_initial_inner_radius": 0.014932033668244029, "grain_initial_height": 0.11986670781368569, "grain_separation": 0.0043804774372666125, "grains_center_of_mass_position": 0.39749334004739806, "center_of_dry_mass_position": 0.317, "nozzle_position": 0.00012776739944301812, "throat_radius": 0.011558987272317063, "interpolate": "linear", "coordinate_system_orientation": "nozzle_to_combustion_chamber", "position": -1.2554668494646906}], "aerodynamic_surfaces": [{"length": 0.5585738309196118, "kind": "vonKarman", "base_radius": 0.0635, "bluffness": 0, "rocket_radius": 0.0635, "name": "Nose Cone", "position": [0, 0, 1.133607250248703]}, {"n": 4, "root_chord": 0.11954751546671595, "tip_chord": 0.05966602935963838, "span": 0.10964031934715668, "rocket_radius": 0.0635, "cant_angle": 0.5, "sweep_length": 0.06, "sweep_angle": null, "airfoil": ["../../../data/airfoils/NACA0012-radians.txt", "radians"], "name": "Fins", "position": [0, 0, -1.0514983708842365]}, {"top_radius": 0.06343918078680816, "bottom_radius": 0.04325007199856578, "length": 0.060394317313238605, "rocket_radius": 0.0635, "name": "Tail", "position": [0, 0, [0, 0, -1.194656]]}], "rail_buttons": [{"buttons_distance": 0.6974746622933771, "angular_position": 45, "name": "Rail Buttons", "lower_button_position": -0.6188258915052254, "upper_button_position": 0.07864877078815169}], "rail_length": 5, "inclination": 84.44167248190685, "heading": 54.43860091183173}