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Thermal-powered reciprocating pump
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Sabelman, E. E. |
| Copyright Year | 1972 |
| Description | Waste heat from radioisotope thermal generators in spacecraft is transported to keep instruments warm by two-cylinder reciprocating pump powered by energy from warm heat exchange fluid. Each cylinder has thermally nonconductive piston, heat exchange coil, and heat sink surface. |
| File Size | 120659 |
| Page Count | 2 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19720000722 |
| Archival Resource Key | ark:/13960/t47q3rf1v |
| Language | English |
| Publisher Date | 1972-12-01 |
| Access Restriction | Open |
| Subject Keyword | Reciprocation Pistons Spacecraft Instruments Vaporizing Pumps Thermoelectric Generators Heat Transmission Heat Exchangers Heat Sinks Condensation 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 |