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Ssme/side loads analysis for flight configuration, revision a. [structural analysis of space shuttle main engine under side load excitation
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Holland, W. |
| Copyright Year | 1974 |
| Description | This document describes the dynamic loads analysis accomplished for the Space Shuttle Main Engine (SSME) considering the side load excitation associated with transient flow separation on the engine bell during ground ignition. The results contained herein pertain only to the flight configuration. A Monte Carlo procedure was employed to select the input variables describing the side load excitation and the loads were statistically combined. This revision includes an active thrust vector control system representation and updated orbiter thrust structure stiffness characteristics. No future revisions are planned but may be necessary as system definition and input parameters change. |
| File Size | 3525508 |
| Page Count | 89 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19750002092 |
| Archival Resource Key | ark:/13960/t6sz12p9r |
| Language | English |
| Publisher Date | 1974-09-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Propulsion And Power Numerical Analysis Propulsion System Performance Space Shuttles Shock Loads Thrust Vector Control Rocket Engines Transient Loads Monte Carlo Method Spacecraft Propulsion Structural Analysis 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 |
