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A cooled-gas pyrometer for use in hypersonic engine testing
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Glawe, G. E. |
| Copyright Year | 1973 |
| Description | A cooled-gas pyrometer designed for application in a hypersonic research engine program was fabricated and tested. Design and operational considerations and calibration data are presented. The probe was tested in a rocket-engine exhaust stream operating at Mach 2 and 2300 K. Test temperature measurements agreed to within 2 percent with a radiation shielded thermocouple probe. |
| File Size | 2124302 |
| Page Count | 19 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19730007769 |
| Archival Resource Key | ark:/13960/t1zd2pp2v |
| Language | English |
| Publisher Date | 1973-02-01 |
| Access Restriction | Open |
| Subject Keyword | Equipment Specifications Electronic Equipment Hypersonic Speed Temperature Measuring Instruments Research Projects Rocket Engines Pyrometers Engine Tests Test Equipment 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 |