SUAVE.Attributes.Propellants.Gaseous_H2.Gaseous_H2 Class Reference

Inheritance diagram for SUAVE.Attributes.Propellants.Gaseous_H2.Gaseous_H2:

Public Member Functions
def	__defaults__ (self)

Public Attributes
	tag
	reactant
	specific_energy
	energy_density
	max_mass_fraction
	composition
	molecular_mass
	gas_constant
	pressure
	temperature
	compressibility_factor
	density
Public Attributes inherited from SUAVE.Attributes.Propellants.Propellant.Propellant
	tag
	reactant
	density
	specific_energy
	energy_density
	max_mass_fraction
	temperatures

Detailed Description

Holds values for this propellant

Assumptions:
None

Source:
None

Member Function Documentation

__defaults__()

def SUAVE.Attributes.Propellants.Gaseous_H2.Gaseous_H2.__defaults__

(

self

)

This sets the default values.

Assumptions:
None

Source:
Values commonly available

Inputs:
None

Outputs:
None

Properties Used:
None

Reimplemented from SUAVE.Attributes.Propellants.Propellant.Propellant.

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The documentation for this class was generated from the following file:

• /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Attributes/Propellants/Gaseous_H2.py