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Isotope brayton space power systems and their technology
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Schwartz, H. |
| Copyright Year | 1972 |
| Description | The objectives of the NASA Brayton Space Power Program and the advantages of achieving an isotope Brayton space power system are enumerated. The paper describes the 2-15 kWe Brayton engine, its subsystems, and major components and summarizes the status of the test program. Two areas of Brayton constituent technology are discussed-gas bearings and heat exchangers. A summary is given of a 500-2500 W isotope Brayton space power system study that showed very attractive performance, simplicity, and low cost for a system in this power range. |
| File Size | 2889235 |
| Page Count | 21 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19730006354 |
| Archival Resource Key | ark:/13960/t2k697q88 |
| Language | English |
| Publisher Date | 1972-01-01 |
| Access Restriction | Open |
| Subject Keyword | Auxiliary Systems Nasa Programs Performance Tests Cost Effectiveness Radioactive Isotopes Gas Turbine Engines Brayton Cycle Engine Parts Space Power Reactors Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |