backend.routers.flight.PropellantDiagnostics Class Reference

Inheritance diagram for backend.routers.flight.PropellantDiagnostics:

Collaboration diagram for backend.routers.flight.PropellantDiagnostics:

Static Public Attributes
str	regime = Field(description="truncated | full_burn | excess_propellant")
Optional	lox_tank_max_kg = None
Optional	fuel_tank_max_kg = None
Optional	target_apogee_m = None
Optional	propellant_tank_fill_factor
Optional	mass_caps = None
List	warnings = Field(default_factory=list)

Detailed Description

Propellant vs time-series requirements for flight iteration.

Definition at line 197 of file flight.py.

Member Data Documentation

fuel_tank_max_kg

Optional backend.routers.flight.PropellantDiagnostics.fuel_tank_max_kg = None

static

Definition at line 210 of file flight.py.

lox_tank_max_kg

Optional backend.routers.flight.PropellantDiagnostics.lox_tank_max_kg = None

static

Definition at line 209 of file flight.py.

mass_caps

Optional backend.routers.flight.PropellantDiagnostics.mass_caps = None

static

Definition at line 215 of file flight.py.

propellant_tank_fill_factor

Optional backend.routers.flight.PropellantDiagnostics.propellant_tank_fill_factor

static

Initial value:

=  Field(
        default=None, description="Fill fraction used for tank volume mass caps"
    )

Definition at line 212 of file flight.py.

regime

str backend.routers.flight.PropellantDiagnostics.regime = Field(description="truncated | full_burn | excess_propellant")

static

Definition at line 199 of file flight.py.

target_apogee_m

Optional backend.routers.flight.PropellantDiagnostics.target_apogee_m = None

static

Definition at line 211 of file flight.py.

warnings

List backend.routers.flight.PropellantDiagnostics.warnings = Field(default_factory=list)

static

Definition at line 216 of file flight.py.

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

• EngineDesign/backend/routers/flight.py