flight.py File Reference

Go to the source code of this file.

Classes
class	engine.layerx.flight.InlineAscent

Namespaces
namespace	engine
namespace	engine.layerx
namespace	engine.layerx.flight

Functions
Optional[float]	engine.layerx.flight._drawn_length_m (Dict[str, Any] edge)
List[str]	engine.layerx.flight._path_to_tank (Any model, str inlet, str tank)
Optional[float]	engine.layerx.flight._elevation_m (Dict[str, Any] edge)
List[Dict[str, Any]]	engine.layerx.flight.line_paths (Dict[str, Any] payload, Any model, Dict[str, str] inlets, Dict[str, str] tanks, Sequence[str] restated)
Optional[str]	engine.layerx.flight.coolprop_gas (Optional[str] name)
Any	engine.layerx.flight._flight_config (Any config, Optional[Dict[str, Any]] timeseries, Dict[str, float] loads, float ambient_pa, Optional[float] pressurant_kg, Optional[float] copv_volume_L, List[str] notes, Optional[str] pressurant_gas=None)
Optional[float]	engine.layerx.flight.config_dry_kg (Any config)
Optional[Dict[str, Any]]	engine.layerx.flight._ceiling (Any config, float apogee_agl, float elevation)
float	engine.layerx.flight._axial_drag (Any flight, float t)
float	engine.layerx.flight.axial_acceleration (Any flight, float t)
Dict[str, Any]	engine.layerx.flight._cfg_input (Any section, str field, str unit, str where)
Dict[str, Any]	engine.layerx.flight.vehicle_stability (Any flight, Any config, Sequence[float] clock)
Dict[str, Any]	engine.layerx.flight._stability_or_failure (Any flight, Any config, Sequence[float] clock, Optional[Dict[str, Any]] scalars)
Tuple[float, float, float, Any]	engine.layerx.flight._vehicle_terms (Any config, Any drag=None)
Dict[str, Any]	engine.layerx.flight.inline_specific_force (Any config, Sequence[float] thrust_N, Sequence[float] mdot_total, Sequence[float] t, float liftoff_mass_kg, float ambient_pa, *, Any drag=None, float dt_max=0.01)
Dict[str, Any]	engine.layerx.flight.liftoff_mass (Any config, Dict[str, float] loads, *, float ambient_pa=101325.0, Optional[float] pressurant_kg=None, Optional[float] copv_volume_L=None, Optional[float] ullage_gas_kg=None, Optional[str] pressurant_gas=None, Optional[float] weighed_kg=None)
Dict[str, Any]	engine.layerx.flight.fly (Any config, Dict[str, Any] timeseries, Dict[str, float] loads, float ambient_pa, *, Optional[float] pressurant_kg=None, Optional[float] copv_volume_L=None, Optional[float] liftoff_mass_kg=None, Optional[float] ullage_gas_kg=None, Optional[str] pressurant_gas=None)
float	engine.layerx.flight.schedule_change (Optional[Dict[str, Any]] old, Optional[Dict[str, Any]] new)

Variables
float	engine.layerx.flight.G0 = 9.80665
int	engine.layerx.flight.ACCEL_TOLERANCE = 5e-3
int	engine.layerx.flight.MAX_FLIGHT_PASSES = 4
int	engine.layerx.flight.TRAJECTORY_POINTS = 240
dict	engine.layerx.flight._TO_M = {"m": 1.0, "mm": 1e-3, "cm": 1e-2, "in": 0.0254, "ft": 0.3048}
tuple	engine.layerx.flight.STABILITY_SOURCE
tuple	engine.layerx.flight.INLINE_SOURCE