backend.routers.flight.FlightSimResponse Class Reference

Inheritance diagram for backend.routers.flight.FlightSimResponse:

Collaboration diagram for backend.routers.flight.FlightSimResponse:

Static Public Attributes
float	apogee_m = Field(description="Apogee AGL [m]")
float	apogee_ft = Field(description="Apogee AGL [ft]")
float	max_velocity_m_s = Field(description="Maximum velocity [m/s]")
float	flight_time_s = Field(description="Total flight time [s]")
Optional	trajectory = Field(default=None, description="Flight trajectory data")
Optional	truncation = Field(default=None, description="Truncation info")
Optional	propellant = Field(default=None, description="Propellant diagnostics")
Optional	thrust_curve = Field(default=None, description="Thrust curve used (time, thrust arrays)")
Optional	rocket_diagram = Field(default=None, description="Base64-encoded rocket diagram PNG")
Optional	error = Field(default=None, description="Error message if failed")
Optional	apogee_msl_m = Field(default=None, description="Apogee above sea level [m]")
Optional	max_mach = Field(default=None, description="Maximum Mach number")
Optional	rail_exit_velocity_m_s = Field(default=None, description="Velocity leaving the rail [m/s]")
Optional	static_margin_rail_exit_cal = Field(default=None, description="Static margin at rail exit [cal]")
Optional	static_margin_burnout_cal = Field(default=None, description="Static margin at burnout [cal]")
Optional	ceiling = Field(default=None, description="Apogee ceiling check (design_requirements.max_apogee_m); None when unset")
Optional	report = Field(default=None, description="Flight report: launch, stability, drag Cd(M) and its inputs, ullage, checks, warnings")

Detailed Description

Response for flight simulation.

Definition at line 219 of file flight.py.

Member Data Documentation

apogee_ft

float backend.routers.flight.FlightSimResponse.apogee_ft = Field(description="Apogee AGL [ft]")

static

Definition at line 223 of file flight.py.

apogee_m

float backend.routers.flight.FlightSimResponse.apogee_m = Field(description="Apogee AGL [m]")

static

Definition at line 222 of file flight.py.

apogee_msl_m

Optional backend.routers.flight.FlightSimResponse.apogee_msl_m = Field(default=None, description="Apogee above sea level [m]")

static

Definition at line 232 of file flight.py.

ceiling

Optional backend.routers.flight.FlightSimResponse.ceiling = Field(default=None, description="Apogee ceiling check (design_requirements.max_apogee_m); None when unset")

static

Definition at line 237 of file flight.py.

error

Optional backend.routers.flight.FlightSimResponse.error = Field(default=None, description="Error message if failed")

static

Definition at line 231 of file flight.py.

Referenced by backend.routers.layerx.Job.view().

flight_time_s

float backend.routers.flight.FlightSimResponse.flight_time_s = Field(description="Total flight time [s]")

static

Definition at line 225 of file flight.py.

max_mach

Optional backend.routers.flight.FlightSimResponse.max_mach = Field(default=None, description="Maximum Mach number")

static

Definition at line 233 of file flight.py.

max_velocity_m_s

float backend.routers.flight.FlightSimResponse.max_velocity_m_s = Field(description="Maximum velocity [m/s]")

static

Definition at line 224 of file flight.py.

propellant

Optional backend.routers.flight.FlightSimResponse.propellant = Field(default=None, description="Propellant diagnostics")

static

Definition at line 228 of file flight.py.

rail_exit_velocity_m_s

Optional backend.routers.flight.FlightSimResponse.rail_exit_velocity_m_s = Field(default=None, description="Velocity leaving the rail [m/s]")

static

Definition at line 234 of file flight.py.

report

Optional backend.routers.flight.FlightSimResponse.report = Field(default=None, description="Flight report: launch, stability, drag Cd(M) and its inputs, ullage, checks, warnings")

static

Definition at line 238 of file flight.py.

rocket_diagram

Optional backend.routers.flight.FlightSimResponse.rocket_diagram = Field(default=None, description="Base64-encoded rocket diagram PNG")

static

Definition at line 230 of file flight.py.

static_margin_burnout_cal

Optional backend.routers.flight.FlightSimResponse.static_margin_burnout_cal = Field(default=None, description="Static margin at burnout [cal]")

static

Definition at line 236 of file flight.py.

static_margin_rail_exit_cal

Optional backend.routers.flight.FlightSimResponse.static_margin_rail_exit_cal = Field(default=None, description="Static margin at rail exit [cal]")

static

Definition at line 235 of file flight.py.

thrust_curve

Optional backend.routers.flight.FlightSimResponse.thrust_curve = Field(default=None, description="Thrust curve used (time, thrust arrays)")

static

Definition at line 229 of file flight.py.

trajectory

Optional backend.routers.flight.FlightSimResponse.trajectory = Field(default=None, description="Flight trajectory data")

static

Definition at line 226 of file flight.py.

truncation

Optional backend.routers.flight.FlightSimResponse.truncation = Field(default=None, description="Truncation info")

static

Definition at line 227 of file flight.py.

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

• EngineDesign/backend/routers/flight.py