Source code for RCAIDE.Library.Attributes.Propellants.Methane

# RCAIDE/Library/Attributes/Propellants/Methane.py
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# Created:  Mar 2024, M. Clarke

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#  Imports
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from .Propellant import Propellant 

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# Methane Propellant Class
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[docs] class Methane(Propellant): """ A class representing methane (CH4) fuel properties and emissions characteristics for propulsion applications. Attributes ---------- tag : str Identifier for the propellant ('Methane') reactant : str Oxidizer used for combustion ('O2') density : float Fuel density in kg/m³ (422.6) specific_energy : float Specific energy content in J/kg (5.34e7) energy_density : float Energy density in J/m³ (2.26e10) lower_heating_value : float Lower heating value in J/kg (5.0e7) use_high_fidelity_kinetics_model : bool Flag for using detailed chemical kinetics (False) fuel_surrogate_chemical_properties : dict Simplified chemical composition {'CH4': 1.0} fuel_chemical_properties : dict Detailed chemical composition {'CH4': 1.0} air_chemical_properties : dict Air composition for combustion calculations {'O2': 0.2095, 'N2': 0.7809, 'AR': 0.0096} global_warming_potential_100 : Data 100-year global warming potentials - CO2 : float Carbon dioxide (1) - H2O : float Water vapor (0.06) - SO2 : float Sulfur dioxide (-226) - NOx : float Nitrogen oxides (52) - Soot : float Particulate matter (1166) - Contrails : float Contrail formation (11) Notes ----- Methane is the simplest hydrocarbon fuel and main component of natural gas. It offers reduced carbon emissions compared to conventional fuels due to its high hydrogen-to-carbon ratio. **Definitions** 'Lower Heating Value' Heat of combustion excluding latent heat of water vapor 'Global Warming Potential' Relative measure of heat trapped in atmosphere compared to CO2 'Specific Energy' Energy content per unit mass, higher than conventional jet fuels **Major Assumptions** * Properties are for standard temperature and pressure conditions (15C, 1atm) * Pure methane composition (no higher hydrocarbons) * Standard atmospheric composition for air """ def __defaults__(self): """This sets the default values. Assumptions: Density at -162C, 1 atm Source: """ self.tag = 'Methane' self.reactant = 'O2' self.density = 422.6 # kg/m^3 (15 C, 1 atm) self.specific_energy = 5.34e7 # J/kg self.energy_density = 2.26e10 # J/m^3 self.lower_heating_value = 5.0e7 # J/kg self.stoichiometric_fuel_air_ratio = 0 # [-] Stoichiometric Fuel to Air ratio self.heat_of_vaporization = 0 # [J/kg] Heat of vaporization at standard conditions self.temperature = 0 # [K] Temperature of fuel self.pressure = 0 # [Pa] Pressure of fuel self.fuel_surrogate_S1 = {} # [-] Mole fractions of fuel surrogate species self.kinetic_mechanism = '' # [-] Kinetic mechanism for fuel surrogate species self.oxidizer = '' self.global_warming_potential_100.CO2 = 1 # CO2e/kg self.global_warming_potential_100.H2O = 0.06 # CO2e/kg self.global_warming_potential_100.SO2 = -226 # CO2e/kg self.global_warming_potential_100.NOx = 52 # CO2e/kg self.global_warming_potential_100.Soot = 1166 # CO2e/kg self.global_warming_potential_100.Contrails = 11 # kg/CO2e/km