Loading...
Please wait, while we are loading the content...
Similar Documents
A comparison of high cycle fatigue methodologies
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Herda, D. A. |
| Copyright Year | 1992 |
| Description | To evaluate alternate turbopump development (ATD) high cycle fatigue (HCF) methodology, a comparison was made with the space shuttle main engine (SSME) methodology. This report documents the comparison and evaluates ATD's HCF system. |
| File Size | 702118 |
| Page Count | 20 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930002960 |
| Archival Resource Key | ark:/13960/t7xm3782w |
| Language | English |
| Publisher Date | 1992-08-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Propulsion And Power Fatigue Life Turbine Pumps Engine Design Fatigue Materials Space Shuttle Main Engine Cyclic Loads 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 |