Public Member Functions
	__init__ (self, PintleEngineConfig base_config)
Dict[str, Any]	optimize_vehicle (self, Dict[str, Any] vehicle_requirements, Optional[Dict[str, Any]] constraints=None)

Public Attributes
	base_config = base_config
	pintle_optimizer = ComprehensivePintleOptimizer(base_config)

Detailed Description

Vehicle-level optimizer that couples flight simulation with engine optimization.

Takes vehicle requirements (altitude, payload, constraints) and optimizes:
- Propellant masses
- Tank sizes
- Engine geometry (via ComprehensivePintleOptimizer)
- COPV sizing

Definition at line 347 of file comprehensive_optimizer.py.

Constructor & Destructor Documentation

◆ init()

engine.pipeline.comprehensive_optimizer.VehicleLevelOptimizer.__init__	(		self,
		PintleEngineConfig	base_config )

Definition at line 358 of file comprehensive_optimizer.py.

Member Function Documentation

◆ optimize_vehicle()

Dict[str, Any] engine.pipeline.comprehensive_optimizer.VehicleLevelOptimizer.optimize_vehicle	(		self,
		Dict[str, Any]	vehicle_requirements,
		Optional[Dict[str, Any]]	constraints = None )

Optimize complete vehicle design.

Parameters:
-----------
vehicle_requirements : dict
    - target_altitude: float [m]
    - payload_mass: float [kg]
    - max_length: float [m]
    - max_diameter: float [m]
    - recovery_system_mass: float [kg]
    - avionics_mass: float [kg]
    - constraints: dict with bounds

Returns:
--------
results : dict
    Optimized vehicle configuration

Definition at line 362 of file comprehensive_optimizer.py.

References engine.pipeline.chamber_optimizer.ChamberOptimizer.base_config, engine.pipeline.comprehensive_optimizer.ComprehensivePintleOptimizer.base_config, and base_config.