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Ames heat pipe experiment (ahpe) experiment description document. [performance testing in a vacuum environment
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Marcus, B. D. |
| Copyright Year | 1972 |
| Description | A gas-controlled variable-conductance heat pipe was qualified for flight aboard orbiting astronomical observatory (OAO3). Experiments were conducted to determine the performance and reliability of the pipe in the vacuum environment of space, and to demonstrate in a specific engineering application its effectiveness in providing temperature stability for spacecraft equipment which experiences varying electronic duty cycles and changing thermal boundary conditions. System design and hardware are discussed in detail. |
| File Size | 4185114 |
| Page Count | 76 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19750015808 |
| Archival Resource Key | ark:/13960/t7gr1pb75 |
| Language | English |
| Publisher Date | 1972-01-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Heat Transfer Conductive Heat Transfer Performance Tests Heat Pipes Oao 3 Vacuum Tests Temperature Control Design Analysis Load Tests 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 |