{
    "rocket_name": "Example Rocket",
    "description": "Sample configuration for testing and demonstration",
    "dimensions": {
        "length": 3.5,
        "diameter": 0.152,
        "fin_span": 0.3,
        "nose_cone_length": 0.4
    },
    "mass_properties": {
        "dry_mass": 15.2,
        "propellant_mass": 8.5,
        "center_of_gravity": 1.8,
        "center_of_pressure": 2.1
    },
    "file_paths": {
        "motor_file": "data/motors/example_motor.csv",
        "aero_file": "data/aero/example_drag_profile.csv"
    },
    "simulation_parameters": {
        "time_step": 0.01,
        "max_simulation_time": 300,
        "launch_angle": 90,
        "launch_altitude": 0,
        "wind_speed": 5.0,
        "wind_direction": 270
    },
    "active_drag_system": {
        "enabled": true,
        "activation_altitude": 1000,
        "target_apogee": 3048,
        "control_frequency": 10,
        "max_drag_coefficient": 2.5,
        "min_drag_coefficient": 0.5
    }
}