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BEACON eSpace at Jet Propulsion Laboratory >
JPL Technical Report Server >
JPL TRS 1992+ >
Please use this identifier to cite or link to this item:
http://hdl.handle.net/2014/22302
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Full metadata record
| DC Field | Value | Language |
|---|
| dc.contributor.author | Tsurutani, B. T. | en_US |
| dc.date.accessioned | 2004-09-26 | - |
| dc.date.available | 2004-09-26 | - |
| dc.date.issued | 1997 | - |
| dc.identifier.clearanceno | 97-0777 | - |
| dc.identifier.uri | http://hdl.handle.net/2014/22302 | - |
| dc.description.abstract | The Solar Probe Mission will be developed under the NASA Outer Planets Program using X-2000 system technology. The present design uses non-nuclear power systems, with the prime mission from 0.5 AU on the inbound pass, to a perihelion of 4Rs, to 0.5 AU on the outbound pass. | en_US |
| dc.format.extent | 103026 bytes | - |
| dc.format.mimetype | application/pdf | - |
| dc.language.iso | en_US | - |
| dc.subject.other | plasma processes | en_US |
| dc.title | The JPL/NASA Solar Probe Mission | en_US |
| Appears in Collections: | JPL TRS 1992+
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