NASA NTRS ยท 19670000624
Propellant tank pressurization analysis program
Abstract
Computer program for the analysis of a single propellant tank pressurization system includes many pertinent physical phenomena previously ignored in other mathematical models. This program can be used for analysis, simulation, and design of propellant pressurization systems.
Keep this discovery
Explore connections, maps & timelines
Epstein, M.. 1967-12-01. Propellant tank pressurization analysis program. https://ntrs.nasa.gov/citations/19670000624
Cite the original work for its findings. Save a collection to share your selection of sources.