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Modeling of space vehicle propellant mixing. [cryogenic propellants]
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Aydelott, J. C. |
| Copyright Year | 1983 |
| Description | An experimental program was conducted to examine the liquid flow patterns that result from the axial-jet mixing of ethanol in 10-cm-diameter spherical and cylindrical containers under zero-, reduced-, and normal-gravity conditions. Dimensionless parameters were developed that characterized the observed liquid flow patterns and the bulk-liquid mixing phenomena. The correlations developed, were used to analyze a typical liquid hydrogen tank and internal thermodynamic vent system for a shuttle-compatible space tug similar to current orbit transfer vehicle concepts. |
| File Size | 2002761 |
| Page Count | 30 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19830008274 |
| Archival Resource Key | ark:/13960/t70w39r4b |
| Language | English |
| Publisher Date | 1983-01-01 |
| Access Restriction | Open |
| Subject Keyword | Propellants And Fuels Orbit Transfer Vehicles Jet Mixing Flow Fluid Dynamics Dimensional Analysis Ethyl Alcohol Liquid-vapor Interfaces Propellant Tanks Microgravity High Speed Cameras Cryogenic Rocket Propellants Spacecraft Propulsion Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
