SUAVE  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
SUAVE.Attributes.Propellants.LOX_RP1.LOX_RP1 Class Reference
Inheritance diagram for SUAVE.Attributes.Propellants.LOX_RP1.LOX_RP1:
SUAVE.Attributes.Propellants.Propellant.Propellant

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 2.27


Source:
Sutton, Rocket Propulsion Elements

Member Function Documentation

◆ __defaults__()

def SUAVE.Attributes.Propellants.LOX_RP1.LOX_RP1.__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: