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A small, single stage orifice pulse tube cryocooler demonstration
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Hendricks, John B. |
| Copyright Year | 1990 |
| Description | This final report summarizes and presents the analytical and experimental progress in the present effort. The principal objective of this effort was the demonstration of a 0.25 Watt, 80 Kelvin orifice pulse tube refrigerator. The experimental apparatus is described. The design of a partially optimized pulse tube refrigerator is included. The refrigerator demonstrates an ultimate temperature of 77 K, has a projected cooling power of 0.18 Watts at 80 K, and has a measured cooling power of 1 Watt at 97 K, with an electrical efficiency of 250 Watts/Watt, much better than previous pulse tube refrigerators. A model of the pulse tube refrigerator that provides estimates of pressure ratio and mass flow within the pulse tube refrigerator, based on component physical characteristics is included. A model of a pulse tube operation based on generalized analysis which is adequate to support local optimization of existing designs is included. A model of regenerator performance based on an analogy to counterflow heat exchangers is included. |
| File Size | 2440877 |
| Page Count | 98 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930004216 |
| Archival Resource Key | ark:/13960/t0vq7v57d |
| Language | English |
| Publisher Date | 1990-08-28 |
| Access Restriction | Open |
| Subject Keyword | Refrigerators Pressure Drop Orifices Cryogenic Cooling Performance Prediction Pressure Ratio Regenerators Mathematical Models Heat Exchangers Mass Flow 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 |