Specific Volume at Throat evaluator uses Specific Volume = Inlet Volume*((Specific Heat Ratio+1)/2)^(1/(Specific Heat Ratio-1)) to evaluate the Specific Volume, Specific Volume at Throat formula is defined as a measure of the volume occupied by a unit mass of gas at the throat of a rocket nozzle, which is crucial for understanding the flow characteristics and performance of rocket propulsion systems. Specific Volume is denoted by Vt symbol.
How to evaluate Specific Volume at Throat using this online evaluator? To use this online evaluator for Specific Volume at Throat, enter Inlet Volume (V1) & Specific Heat Ratio (γ) and hit the calculate button.