Publication Date:
2019-07-13
Description:
This paper describes a computational model of the chilldown and propellant loading of the Space Shuttle External Tank liquid oxygen and hydrogen tanks at Launch Complex 39B at Kennedy Space Center. The purpose of the computational model is to predict the time required to chilldown the entire assembly consisting of the ground system transfer line and propellant tanks in order to compare with observed loading times, to evaluate the feasibility of similar models developed for the Ares I Upper Stage. The model also predicts the history of inflow and outflow from the tank, pressure and temperature inside the tank, and heat leak through the walls. The Generalized Fluid System Simulation Program (GFSSP), a general purpose network flow analysis code, has been used to develop this computational model. The paper describes the simulation of the loading process for both tanks and compares the resulting predictions to measurements
Keywords:
Spacecraft Design, Testing and Performance
Type:
M10-0816
,
46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit; Jul 25, 2010 - Jul 28, 2010; Nashville, TN; United States
Format:
application/pdf
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