flight_1dof.py File Reference

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Namespaces
namespace	engine
namespace	engine.pipeline
namespace	engine.pipeline.flight_1dof

Functions
float	engine.pipeline.flight_1dof.vertical_apogee_agl (Sequence[float] time_s, Sequence[float] thrust_n, Sequence[float] mdot_kg_s, float m0_kg, *, float area_m2=0.0, Optional[DragCurves] drag=None, float elevation_m=0.0, Optional[float] reference_pressure_pa=None, float nozzle_exit_area_m2=0.0, float dt_burn=0.01, float dt_coast=0.05)
float	engine.pipeline.flight_1dof.required_impulse (float target_apogee_agl_m, float m_dry_kg, float m_prop_kg, float burn_time_s, *, Optional[Sequence[float]] time_s=None, Optional[Sequence[float]] mdot_kg_s=None, Optional[Sequence[float]] thrust_n=None, **object flight)

Variables
float	engine.pipeline.flight_1dof.G0 = 9.80665