NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Due to the lapse in federal government funding, NASA is not updating this website. We sincerely regret this inconvenience.

Back to Results
GUI for Computational Simulation of a Propellant MixerControl Panel is a computer program that generates a graphical user interface (GUI) for computational simulation of a rocket-test-stand propellant mixer in which gaseous hydrogen (GH2) is injected into flowing liquid hydrogen (LH2) to obtain a combined flow having desired thermodynamic properties. The GUI is used in conjunction with software that models the mixer as a system having three inputs (the positions of the GH2 and LH2 inlet valves and an outlet valve) and three outputs (the pressure inside the mixer and the outlet flow temperature and flow rate). The user can specify valve characteristics and thermodynamic properties of the input fluids via userfriendly dialog boxes. The user can enter temporally varying input values or temporally varying desired output values. The GUI provides (1) a set-point calculator function for determining fixed valve positions that yield desired output values and (2) simulation functions that predict the response of the mixer to variations in the properties of the LH2 and GH2 and manual- or feedback-control variations in valve positions. The GUI enables scheduling of a sequence of operations that includes switching from manual to feedback control when a certain event occurs.
Document ID
20110016373
Acquisition Source
Stennis Space Center
Document Type
Other - NASA Tech Brief
Authors
Figueroa, Fernando
(NASA Stennis Space Center Stennis Space Center, MS, United States)
Richter, Hanz
(Cleveland State Univ. Cleveland, OH, United States)
Barbieri, Enrique
(Tulane Univ. New Orleans, LA, United States)
Granger, Jamie
(Tulane Univ. New Orleans, LA, United States)
Date Acquired
August 25, 2013
Publication Date
November 1, 2005
Publication Information
Publication: NASA Tech Briefs, November 2005
Subject Category
Man/System Technology And Life Support
Report/Patent Number
SSC-00213
Report Number: SSC-00213
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available