engine.pipeline.config_schemas.ThrustConfig Class Reference

Inheritance diagram for engine.pipeline.config_schemas.ThrustConfig:

Collaboration diagram for engine.pipeline.config_schemas.ThrustConfig:

Static Public Attributes
float	burn_time = Field(gt=0, description="Burn time [s]")
Optional	reference_pressure_pa = Field(default=None, gt=0, description="Ambient pressure the thrust curve was computed at [Pa]; the flight adds (p_ref - p(z))*A_exit. Unset: compute_ambient_pressure_from_elevation(environment.elevation), the engine solver's own reference.")

Detailed Description

Thrust configuration for flight simulation

Definition at line 1588 of file config_schemas.py.

Member Data Documentation

burn_time

float engine.pipeline.config_schemas.ThrustConfig.burn_time = Field(gt=0, description="Burn time [s]")

static

Definition at line 1590 of file config_schemas.py.

reference_pressure_pa

Optional engine.pipeline.config_schemas.ThrustConfig.reference_pressure_pa = Field(default=None, gt=0, description="Ambient pressure the thrust curve was computed at [Pa]; the flight adds (p_ref - p(z))*A_exit. Unset: compute_ambient_pressure_from_elevation(environment.elevation), the engine solver's own reference.")

static

Definition at line 1591 of file config_schemas.py.

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The documentation for this class was generated from the following file:

• EngineDesign/engine/pipeline/config_schemas.py