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Conceptual definition of a technology development mission for advanced solar dynamic power systems
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Migra, R. P. |
| Copyright Year | 1986 |
| Description | An initial conceptual definition of a technology development mission for advanced solar dynamic power systems is provided, utilizing a space station to provide a dedicated test facility. The advanced power systems considered included Brayton, Stirling, and liquid metal Rankine systems operating in the temperature range of 1040 to 1400 K. The critical technologies for advanced systems were identified by reviewing the current state of the art of solar dynamic power systems. The experimental requirements were determined by planning a system test of a 20 kWe solar dynamic power system on the space station test facility. These requirements were documented via the Mission Requirements Working Group (MRWG) and Technology Development Advocacy Group (TDAG) forms. Various concepts or considerations of advanced concepts are discussed. A preliminary evolutionary plan for this technology development mission was prepared. |
| File Size | 4295504 |
| Page Count | 128 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19870005338 |
| Archival Resource Key | ark:/13960/t7wm65k1f |
| Language | English |
| Publisher Date | 1986-07-01 |
| Access Restriction | Open |
| Subject Keyword | Energy Production And Conversion Test Facilities Stirling Cycle Technology Assessment Rankine Cycle Solar Dynamic Power Systems Spacecraft Power Supplies Liquid Metals Brayton Cycle Design Analysis Space Stations Research Management 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 |
