SUAVE.Attributes.Propellants.Propellant.Propellant Class Reference

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

Public Member Functions
def	__defaults__ (self)

Public Attributes
	tag
	reactant
	density
	specific_energy
	energy_density
	max_mass_fraction
	temperatures

Detailed Description

Holds values for a propellant

Assumptions:
None

Source:
None

Member Function Documentation

__defaults__()

def SUAVE.Attributes.Propellants.Propellant.Propellant.__defaults__

(

self

)

This sets the default values.

Assumptions:
None

Source:
Values commonly available

Inputs:
None

Outputs:
None

Properties Used:
None

Reimplemented in SUAVE.Attributes.Propellants.LOX_LH2.LOX_LH2, SUAVE.Attributes.Propellants.Jet_A.Jet_A, SUAVE.Attributes.Propellants.Jet_A1.Jet_A1, SUAVE.Attributes.Propellants.Liquid_H2.Liquid_H2, SUAVE.Attributes.Propellants.LOX_RP1.LOX_RP1, SUAVE.Attributes.Propellants.Aviation_Gasoline.Aviation_Gasoline, SUAVE.Attributes.Propellants.Gaseous_H2.Gaseous_H2, SUAVE.Attributes.Propellants.JP7.JP7, and SUAVE.Attributes.Propellants.Liquid_Natural_Gas.Liquid_Natural_Gas.

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

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