Source code for RCAIDE.Framework.Analyses.Weights.Hybrid

# RCAIDE/Framework/Analyses/Weights/Hydrogen.py
#
# Created:  Feb 2025, S. Shekar
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#  IMPORT
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import RCAIDE
from RCAIDE.Framework.Core import Data 
from .Weights import Weights

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#  
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class Hybrid(Weights):
    """ This is class that evaluates the weight of lass aircraft

    Assumptions:
        None

    Source:
        N/A

    Inputs:
        None

    Outputs:
        None

    Properties Used:
         N/A
    """

    def __defaults__(self):
        """This sets the default values and methods for the tube and wing
        aircraft weight analysis.

        Assumptions:
        None

        Source:
        N/A

        Inputs:
        None

        Outputs:
        None

        Properties Used:
        N/A
        """

        # self.method        = 'Semi_Emperical'
        # self.aircraft_type = 'Transport'
        # self.propulsion_architecture = 'Hydrogen'