SUAVE.Attributes.Propellants.LOX_LH2.LOX_LH2 Class Reference

Inheritance diagram for SUAVE.Attributes.Propellants.LOX_LH2.LOX_LH2:

Public Member Functions
def	__defaults__ (self)

Public Attributes
	tag
	molecular_weight
	isentropic_expansion_factor
	combustion_temperature
	gas_specific_constant
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:
At an O/F ratio 5.50


Source:
Sutton, Rocket Propulsion Elements
Using CEA

Member Function Documentation

__defaults__()

def SUAVE.Attributes.Propellants.LOX_LH2.LOX_LH2.__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.

---

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

• /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Attributes/Propellants/LOX_LH2.py