How to Calculate Specific Volume at Throat?
Specific Volume at Throat calculator uses Specific Volume = Inlet Volume*((Specific Heat Ratio+1)/2)^(1/(Specific Heat Ratio-1)) to calculate the Specific Volume, The specific volume at throat of a rocket nozzle represents the volume occupied by a unit mass of propellant at that specific location, this formula provides a simplified relationship between the specific volume at the throat and the specific volume at the nozzle exit, taking into account the properties of the gas and the flow conditions within the rocket nozzle. Specific Volume is denoted by V_{t} symbol.
How to calculate Specific Volume at Throat using this online calculator? To use this online calculator for Specific Volume at Throat, enter Inlet Volume (V_{1}) & Specific Heat Ratio (γ) and hit the calculate button. Here is how the Specific Volume at Throat calculation can be explained with given input values -> 10.00756 = 6.3*((1.33+1)/2)^(1/(1.33-1)).