RCAIDE.Library.Attributes.Propellants.Propellant
Propellant#
- class Propellant(*args, **kwarg)[source]#
Bases:
Data
Base class for defining propellant properties and characteristics in propulsion systems.
- tag#
Identifier for the specific propellant type
- Type:
str
- reactant#
Primary oxidizer used for combustion
- Type:
str
- density#
Fuel density in kg/m³
- Type:
float
- specific_energy#
Specific energy content in J/kg
- Type:
float
- energy_density#
Energy density in J/m³
- Type:
float
- lower_heating_value#
Lower heating value in J/kg
- Type:
float
- mass_properties#
Object containing mass-related properties
- Type:
- max_mass_fraction#
- Maximum fuel-to-oxidizer mass ratios
- Airfloat
Maximum mass fraction with air
- O2float
Maximum mass fraction with pure oxygen
- Type:
- temperatures#
- Critical temperatures in K
- flashfloat
Flash point temperature
- autoignitionfloat
Autoignition temperature
- freezefloat
Freezing point temperature
- boilingfloat
Boiling point temperature
- Type:
- emission_indices#
- Emission indices in kg/kg fuel
- Productionfloat
CO2 production rate
- CO2float
Carbon dioxide emissions
- H2Ofloat
Water vapor emissions
- SO2float
Sulfur dioxide emissions
- NOxfloat
Nitrogen oxides emissions
- Sootfloat
Particulate matter emissions
- Type:
- global_warming_potential_100#
- 100-year global warming potentials
- CO2float
Carbon dioxide impact
- H2Ofloat
Water vapor impact
- SO2float
Sulfur dioxide impact
- NOxfloat
Nitrogen oxides impact
- Sootfloat
Particulate matter impact
- Contrailsfloat
Contrail formation impact
- Type:
Notes
This base class provides a standardized structure for defining propellant properties, including physical characteristics, combustion parameters, and environmental impacts. It serves as a template for specific propellant implementations.
Definitions
- ‘Emission Index’
Mass of pollutant produced per unit mass of fuel burned
- ‘Global Warming Potential’
Relative measure of heat trapped in atmosphere compared to CO2
- ‘Lower Heating Value’
Heat of combustion excluding latent heat of water vapor