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Determination of the relative resistance to ignition of selected turbopump materials in high-pressure, high-temperature, oxygen environments, volume 1
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Stoltzfus, Joel M. Benz, Frank J. |
| Copyright Year | 1986 |
| Description | Advances in the design of the liquid oxygen, liquid hydrogen engines for the Space Transportation System call for the use of warm, high-pressure oxygen as the driving gas in the liquid oxygen turbopump. The NASA Lewis Research Center requested the NASA White Sands Test Facility (WSTF) to design a test program to determine the relative resistance to ignition of nine selected turbopump materials: Hastelloy X, Inconel 600, Invar 36, Monel K-500, nickel 200, silicon carbide, stainless steel 316, and zirconium copper. The materials were subjected to particle impact and to frictional heating in high-pressure oxygen. |
| File Size | 7781138 |
| Page Count | 75 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19890006632 |
| Archival Resource Key | ark:/13960/t6838pq4m |
| Language | English |
| Publisher Date | 1986-07-21 |
| Access Restriction | Open |
| Subject Keyword | Inorganic And Physical Chemistry Nickel Alloys Engine Design Monel Trademark Ignition Silicon Carbides Impact Tests Spacecraft Construction Materials Stainless Steels Inconel Trademark Friction Copper Alloys Hydrogen Oxygen Engines Space Transportation System Hastelloy Trademark 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 |
