JIMO follow-on mission studies

被引:0
|
作者
Satter, CM [1 ]
机构
[1] CALTECH, Jet Prop Lab, Pasadena, CA 91001 USA
来源
SPACE TECHNOLOGY AND APPLICATIONS INTERNATIONAL FORUM-STAIF 2005 | 2005年 / 746卷
关键词
D O I
暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Team Prometheus is a geographically-distributed, collaborative engineering team composed of representatives from several NASA centers and the Department of Energy (DOE). During the months of April through September 2004, Team Prometheus performed studies of representative Saturn/Titan and Neptune/Triton science missions based on proposed Jupiter Icy Moons Orbiter (JIMO) technology. The principal objectives of these studies were: 1) to assess the feasibility of using direct copies of the baseline JIMO flight system designs to perform these follow-on missions, and 2) to identify and assess technologies or potential enhancements or alterations to the baseline JIMO designs which could reduce the cruise durations to meet NASA Headquarters-specified programmatic goals. A tertiary objective was to provide feedback to the JIMO Project on the suitability of the JIMO reference designs for potential follow-on applications.
引用
收藏
页码:249 / 257
页数:9
相关论文
共 50 条
  • [1] Status of the GRACE Follow-On Mission
    Flechtner, Frank
    Morton, Phil
    Watkins, Mike
    Webb, Frank
    GRAVITY, GEOID AND HEIGHT SYSTEMS, 2014, 141 : 117 - 121
  • [2] Simulation study of a follow-on gravity mission to GRACE
    Bryant D. Loomis
    R. S. Nerem
    S. B. Luthcke
    Journal of Geodesy, 2012, 86 : 319 - 335
  • [3] Possible LISA follow-on mission scientific objectives
    Bender, Peter L.
    Begelman, Mitchell C.
    Gair, Jonathan R.
    CLASSICAL AND QUANTUM GRAVITY, 2013, 30 (16)
  • [4] TOPEX-POSEIDON - FOLLOW-ON MISSION DESIGN
    MINSTER, JF
    NOUVELLE REVUE AERONAUTIQUE ASTRONAUTIQUE, 1995, (02): : 9 - 14
  • [5] Simulation study of a follow-on gravity mission to GRACE
    Loomis, Bryant D.
    Nerem, R. S.
    Luthcke, S. B.
    JOURNAL OF GEODESY, 2012, 86 (05) : 319 - 335
  • [6] Definition of mission requirements for the follow-on EUMETSAT polar system
    Phillips, P. L.
    Schluessel, P.
    Accadia, C. J.
    Munro, R.
    Wilson, J. J. W.
    Perez-Albinana, A.
    Banfi, S.
    SENSORS, SYSTEMS, AND NEXT-GENERATION SATELLITES XI, 2007, 6744 : 74405 - 74405
  • [7] Advanced design concepts for a SeaWinds scatterometer follow-on mission
    Spencer, MW
    Huddleston, JN
    Stiles, BW
    2001 IEEE AEROSPACE CONFERENCE PROCEEDINGS, VOLS 1-7, 2001, : 1833 - 1839
  • [8] Laser link acquisition demonstration for the GRACE Follow-On mission
    Wuchenich, Danielle M. R.
    Mahrdt, Christoph
    Sheard, Benjamin S.
    Francis, Samuel P.
    Spero, Robert E.
    Miller, John
    Mow-Lowry, Conor M.
    Ward, Robert L.
    Klipstein, William M.
    Heinzel, Gerhard
    Danzmann, Karsten
    McClelland, David E.
    Shaddock, Daniel A.
    OPTICS EXPRESS, 2014, 22 (09): : 11351 - 11366
  • [9] The Odin project -: Lessons for a follow-on earth observation mission
    von Schéele, F
    ACTA ASTRONAUTICA, 2003, 53 (4-10) : 739 - 747
  • [10] Intersatellite laser ranging instrument for the GRACE follow-on mission
    Sheard, B. S.
    Heinzel, G.
    Danzmann, K.
    Shaddock, D. A.
    Klipstein, W. M.
    Folkner, W. M.
    JOURNAL OF GEODESY, 2012, 86 (12) : 1083 - 1095