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Use of higher fidelity slosh models to reduce conservatism in launch vehicle flight control designs
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Hall, Robert A. |
| Copyright Year | 2015 |
| File Size | 774685 |
| Page Count | 14 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20150021445 |
| Archival Resource Key | ark:/13960/t91889h4r |
| Language | English |
| Publisher Date | 2015-10-02 |
| Access Restriction | Open |
| Subject Keyword | Propellants And Fuels Spacecraft Design, Testing And Performance Attitude Inclination Fuel Tanks Propellants Launch Vehicles Pendulums Liquid Oxygen Spacecraft Stability Flight Control Liquid Sloshing Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Presentation |