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The center vent shape for venting a tank in a low gravity environment
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Perkins, C. K. |
| Organization | The National Aeronautics and Space Administration (NASA) |
| Copyright Year | 1961 |
| Description | Center vent tube effect on zero gravity equilibrium configuration for Centaur launch vehicle, second stage liquid propellant tank ullage |
| File Size | 812222 |
| File Format | |
| Alternate Webpage(s) | http://www.archive.org/details/nasa_techdoc_19660020000 |
| Archival Resource Key | ark:/13960/t3gx50z0q |
| Language | English |
| Publisher Date | 1961-07-25 |
| Access Restriction | Open |
| Subject Keyword | Weightlessness Second Stage Propellant Tank Liquid Propellant Centaur Launch Vehicle Venting Vents Launch Vehicles Liquid Rocket Propellants Microgravity Propellant Tanks Propellants Shapes Ullage Upper Stage Rocket Engines Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |