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Materials for advanced rocket engine turbopump turbine blades
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Chandler, W. T. |
| Copyright Year | 1985 |
| Description | A study program was conducted to identify those materials that will provide the greatest benefits as turbine blades for advanced liquid propellant rocket engine turbines and to prepare technology plans for the development of those materials for use in the 1990 through 1995 period. The candidate materials were selected from six classes of materials: single-crystal (SC) superalloys, oxide dispersion-strengthened (ODS) superalloys, rapid solidification processed (RSP) superalloys, directionally solidified eutectic (DSE) superalloys, fiber-reinforced superalloy (FRS) composites, and ceramics. Properties of materials from the six classes were compiled and evaluated and property improvements were projected approximately 5 years into the future for advanced versions of materials in each of the six classes. |
| File Size | 898771 |
| Page Count | 23 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19850018561 |
| Archival Resource Key | ark:/13960/t76t5jg8h |
| Language | English |
| Publisher Date | 1985-04-01 |
| Access Restriction | Open |
| Subject Keyword | Metallic Materials Single Crystals Stress Analysis Turbine Pumps Turbine Blades Heat Resistant Alloys Fatigue Materials Mechanical Properties Liquid Propellant Rocket Engines Solidification Oxide Dispersion Strengthening 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 | Article |
