NASA NTRS · 19690000007
Propellant tank pressurization analysis program
Abstract
Propellant tank pressurization analysis program considers fluid densities related to pressures and temperatures acting on the components, heat transfer between the fluids, the components, the ambient, plus component volumes, materials, and configurations in the formation of a mathematical model. This program is written in FORTRAN H and MAP.
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Epstein, M.. 1969-01-01. Propellant tank pressurization analysis program. https://ntrs.nasa.gov/citations/19690000007
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