backend.routers.flight.FlightSimRequest Class Reference

Inheritance diagram for backend.routers.flight.FlightSimRequest:

Collaboration diagram for backend.routers.flight.FlightSimRequest:

Static Public Attributes
List	time_array = Field(..., min_length=2, description="Time array [s]")
List	thrust_array = Field(..., min_length=2, description="Thrust array [N]")
List	mdot_O_array = Field(..., min_length=2, description="LOX mass flow array [kg/s]")
List	mdot_F_array = Field(..., min_length=2, description="Fuel mass flow array [kg/s]")
float	lox_mass_kg = Field(default=18.0, gt=0, description="Initial LOX mass [kg]")
float	fuel_mass_kg = Field(default=4.0, gt=0, description="Initial fuel mass [kg]")
Optional	lox_tank = Field(default=None, description="LOX tank configuration")
Optional	fuel_tank = Field(default=None, description="Fuel tank configuration")
Optional	environment = Field(default=None, description="Environment configuration")
Optional	rocket = Field(default=None, description="Rocket configuration")
Optional	reference_pressure_pa

Detailed Description

Request body for flight simulation (time-series mode only).

Definition at line 145 of file flight.py.

Member Data Documentation

environment

Optional backend.routers.flight.FlightSimRequest.environment = Field(default=None, description="Environment configuration")

static

Definition at line 162 of file flight.py.

fuel_mass_kg

float backend.routers.flight.FlightSimRequest.fuel_mass_kg = Field(default=4.0, gt=0, description="Initial fuel mass [kg]")

static

Definition at line 155 of file flight.py.

fuel_tank

Optional backend.routers.flight.FlightSimRequest.fuel_tank = Field(default=None, description="Fuel tank configuration")

static

Definition at line 159 of file flight.py.

lox_mass_kg

float backend.routers.flight.FlightSimRequest.lox_mass_kg = Field(default=18.0, gt=0, description="Initial LOX mass [kg]")

static

Definition at line 154 of file flight.py.

lox_tank

Optional backend.routers.flight.FlightSimRequest.lox_tank = Field(default=None, description="LOX tank configuration")

static

Definition at line 158 of file flight.py.

mdot_F_array

List backend.routers.flight.FlightSimRequest.mdot_F_array = Field(..., min_length=2, description="Fuel mass flow array [kg/s]")

static

Definition at line 151 of file flight.py.

mdot_O_array

List backend.routers.flight.FlightSimRequest.mdot_O_array = Field(..., min_length=2, description="LOX mass flow array [kg/s]")

static

Definition at line 150 of file flight.py.

reference_pressure_pa

Optional backend.routers.flight.FlightSimRequest.reference_pressure_pa

static

Initial value:

=  Field(
        default=None, gt=0,
        description="Ambient pressure the thrust curve was computed at [Pa]. Unset: the engine solver's "
                    "reference at the SESSION config's elevation, which is what the time series ran at.")

Definition at line 167 of file flight.py.

rocket

Optional backend.routers.flight.FlightSimRequest.rocket = Field(default=None, description="Rocket configuration")

static

Definition at line 165 of file flight.py.

thrust_array

List backend.routers.flight.FlightSimRequest.thrust_array = Field(..., min_length=2, description="Thrust array [N]")

static

Definition at line 149 of file flight.py.

time_array

List backend.routers.flight.FlightSimRequest.time_array = Field(..., min_length=2, description="Time array [s]")

static

Definition at line 148 of file flight.py.

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

• EngineDesign/backend/routers/flight.py