propulsion

class Propulsion

Bases: CommonBaseModel

Represents the propulsion system within an air vehicle system, detailing its specifications, functionalities, and interrelations.

name

The name of the propulsion system, acting as a unique identifier.

description

A brief description of the propulsion system purpose and functionality.

geometry

Geometric information of the component, if applicable.

parameters

Cycle or physical parameters associated with the propulsion system.

metadata

Additional metadata providing context or details about the propulsion system.

subcomponents

A list of sub-components, if any, within the propulsion system.

requirements

Specific requirements associated with the propulsion system.

performance

List of disciplines analyzing the propulsion system.

behavior

Specific behaviors for the propulsion system.

Raises:: ValueError – If any string field is empty, ensuring all components have meaningful identifiers and descriptions.

Methods:

validate_non_empty_string(value)

Validates that the name and description fields are not empty or whitespace only.

Attributes:

__pydantic_setattr_handlers__

__setattr__ handlers.

classmethod validate_non_empty_string(value)

Validates that the name and description fields are not empty or whitespace only.

Parameters:: value (Optional[str]) – The value to validate.
Returns:: The validated string value.
Return type:: Optional[str]
Raises:: ValueError – If the input value is empty or consists only of whitespace.

class Config

Bases: object

Pydantic model configuration.

__pydantic_setattr_handlers__: ClassVar[Dict[str, Callable[[BaseModel, str, Any], None]]] = {}: __setattr__ handlers. Memoizing the handlers leads to a dramatic performance improvement in __setattr__

Classes

`Propulsion`	Represents the propulsion system within an air vehicle system, detailing its specifications, functionalities, and interrelations.
`PropulsionCycle`	Represents a complete engine cycle.