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A deep space power system option based on synergistic power conversion technologies
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Schreiber, Jeffrey G. |
| Copyright Year | 2000 |
| Description | Deep space science missions have typically used radioisotope thermoelectric generator (RTG) power systems. The RTG power system has proven itself to be a rugged and highly reliable power system over many missions, however the thermal-to-electric conversion technology used was approximately 5% efficient. While the relatively low efficiency has some benefits in terms of system integration, there are compelling reasons why a more efficient conversion system should be pursued. The cost savings alone that are available as a result of the reduced isotope inventory are significant. The Advanced Radioisotope Power System (ARPS) project was established to fulfill this goal. Although it was not part of the ARPS project, Stirling conversion technology is being demonstrated with a low level of funding by both NASA and DOE. A power system with Stirling convertors. although intended for use with an isotope heat source. can be combined with other advanced technologies to provide a novel power system for deep space missions. An inflatable primary concentrator would be used in combination with a refractive secondary concentrator (RSC) as the heat source to power the system. The inflatable technology as a structure has made great progress for a variety of potential applications such as communications reflectors, radiators and solar arrays. The RSC has been pursued for use in solar thermal propulsion applications, and it's unique properties allow some advantageous system trades to be made. The power system proposed would completely eliminate the isotope heat source and could potentially provide power for science missions to planets as distant as Uranus. This paper will present the background and developmental status of the technologies and will then describe the power system being proposed. |
| File Size | 661063 |
| File Format | |
| Language | English |
| Publisher Date | 2000-07-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Propulsion And Power Heat Sources Thermoelectric Power Generation Solar Arrays Deep Space Cost Reduction Thermoelectric Generators Spacecraft Power Supplies Systems Integration Solar Generators Stirling Cycle Solar Thermal Propulsion Technology Transfer Uranus Planet Radioisotope Batteries Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
