The main API for running launch simulations.

Functions¶

solve_to_circular_orbit¶

Solve for optimal circular orbit insertion.

def solve_to_circular_orbit(
    h_target_km: float,
    payload_kg: float,
    *,
    include_trajectory: bool = True,
    trim: bool = True,
    # ... additional parameters
) -> LaunchResult:

Parameters:

Returns: LaunchResult dataclass with: - schema_version: API version - inputs: Echo of input parameters - optimal_numerics: Optimal control values - summary: Mission success metrics - trajectory: Full trajectory data (if requested)

simulate_to_orbit¶

Single simulation with given control parameters.

def simulate_to_orbit(
    h_target_km: float,
    payload_kg: float,
    theta0_deg: float,
    t_coast: float,
    t_burn2: float,
    # ...
) -> Trajectory:

LaunchResult Schema¶

@dataclass
class LaunchResult:
    schema_version: int
    inputs: dict[str, float]
    optimal_numerics: dict[str, float]
    summary: dict[str, float]
    trajectory: dict[str, Any] | None