dc.contributor.author | Dunn, C. | en_US |
dc.contributor.author | Bertiger, W. | en_US |
dc.contributor.author | Franklin, G. | en_US |
dc.contributor.author | Harris, I. | en_US |
dc.contributor.author | Kruizinga, G. | en_US |
dc.contributor.author | Meehan, T. | en_US |
dc.contributor.author | Nandi, S. | en_US |
dc.contributor.author | Nguyen, D. | en_US |
dc.contributor.author | Rogstad, T. | en_US |
dc.contributor.author | Thomas, J. B. | en_US |
dc.contributor.author | Tien, J. | en_US |
dc.date.accessioned | 2004-09-17T18:39:49Z | |
dc.date.available | 2004-09-17T18:39:49Z | |
dc.date.issued | 2002-09-23 | en_US |
dc.identifier.citation | ION 2002 | en_US |
dc.identifier.citation | Portland, OR, USA | en_US |
dc.identifier.clearanceno | 02-2372 | en_US |
dc.identifier.uri | http://hdl.handle.net/2014/10401 | |
dc.description.abstract | This paper will describe the design and on-orbit performance of the GRACE Instrument Processing Unit (IPU) that integrates most of the critical science functions required by the GRACE mission to perform its gravity science and atmospheric radio occultation tasks. | en_US |
dc.format.extent | 569043 bytes | |
dc.format.mimetype | application/pdf | |
dc.language.iso | en_US | |
dc.subject.other | gravity GRACE instrument | en_US |
dc.title | The instrument on NASA's GRACE Mission: Augmentation of GPS to achieve unprecedented gravity field measurements | en_US |