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Ssme structural dynamic model development (Document No: 19840009219)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Welch, C. T. Tilley, D. M. Foley, M. J. |
| Copyright Year | 1983 |
| Description | A mathematical model of the Space Shuttle Main Engine (SSME) as a complete assembly, with detailed emphasis on LOX and High Fuel Turbopumps is developed. The advantages of both complete engine dynamics, and high fidelity modeling are incorporated. Development of this model, some results, and projected applications are discussed. |
| File Size | 14033803 |
| Page Count | 281 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19840009219 |
| Archival Resource Key | ark:/13960/t7jq5t44g |
| Language | English |
| Publisher Date | 1983-12-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Propulsion And Power Turbine Pumps Mathematical Models Engine Design Liquid Oxygen Space Shuttle Main Engine High Pressure 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 |
