backend.routers.flight.TankConfig Class Reference

Inheritance diagram for backend.routers.flight.TankConfig:

Collaboration diagram for backend.routers.flight.TankConfig:

Static Public Attributes
float	mass = Field(..., gt=0, description="Initial propellant mass [kg]")
float	height = Field(default=1.0, gt=0, description="Tank height [m]")
float	radius = Field(default=0.0762, gt=0, description="Tank radius [m]")
float	position = Field(default=0.6, description="Tank position relative to motor [m]")
Optional	volume_m3 = Field(default=None, gt=0, description="Tank volume [m³]. If not provided, will be calculated from height and radius using π×r²×h")

Detailed Description

Tank configuration for flight simulation.

Definition at line 136 of file flight.py.

Member Data Documentation

height

float backend.routers.flight.TankConfig.height = Field(default=1.0, gt=0, description="Tank height [m]")

static

Definition at line 139 of file flight.py.

Referenced by feedtwin.vessels.geometry.CylindricalTank.cross_section(), combined_gui.PressureBarWidget.paintEvent(), feedtwin.vessels.geometry.CylindricalTank.volume_below(), and feedtwin.vessels.geometry.CylindricalTank.wetted_area().

mass

float backend.routers.flight.TankConfig.mass = Field(..., gt=0, description="Initial propellant mass [kg]")

static

Definition at line 138 of file flight.py.

Referenced by feedtwin.comps.wall.LineWall.capacity(), feedtwin.comps.wall.LineWall.capacity_at(), and feedtwin.vessels.volume.VesselState.specific_energy().

position

float backend.routers.flight.TankConfig.position = Field(default=0.6, description="Tank position relative to motor [m]")

static

Definition at line 141 of file flight.py.

radius

float backend.routers.flight.TankConfig.radius = Field(default=0.0762, gt=0, description="Tank radius [m]")

static

Definition at line 140 of file flight.py.

Referenced by feedtwin.vessels.geometry.Head.area_filled(), feedtwin.vessels.geometry.Head.cross_section(), feedtwin.vessels.geometry.Head.depth(), feedtwin.vessels.geometry.Head.volume(), and feedtwin.vessels.geometry.Head.volume_filled().

volume_m3

Optional backend.routers.flight.TankConfig.volume_m3 = Field(default=None, gt=0, description="Tank volume [m³]. If not provided, will be calculated from height and radius using π×r²×h")

static

Definition at line 142 of file flight.py.

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

• EngineDesign/backend/routers/flight.py