Dynamic Simulation of Propellant Utilization System in Propellant Tanks of a Liquid Propellant Engine

M. Naderi Tabrizi; S. A. R. Jalali Chimeh; H. Karimi

Volume 3, Issue 2 , January 2011, , Pages 31-43

Abstract
  In this article the Propellant Utilization system (PU) has been simulated. The objective of this system is to adjust the consumption ratio of the propellants in order to ensure the minimum propellant residuals at engine’s shutdown phase. Using the PU system, the orbital or range and also the payload ...  Read More