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TESSX: A Mission for Space Exploration with TethersTethers offer significant potential for substantially increasing payload mass fraction, increasing spacecraft lifetime, enhancing long-term space travel, and enabling the understanding and development of gravity-dependent technologies required for Moon and Mars exploration. The development of the Tether Electrodynamic Spin-up and Survivability Experiment (TESSX) will support applications relevant to NASA's new exploration initiative, including: artificial gravity generation, formation flying, electrodynamic propulsion, momentum exchange, and multi-amp current collection and emission. Under the broad term TESSX, we are currently evaluating several different tether system configurations and operational modes. The initial results of this work are presented, including hardware development, orbital dynamics simulations, and electrodynamics design and analysis.
Document ID
20050206332
Acquisition Source
Marshall Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Cosmo, Mario L.
(Harvard-Smithsonian Center for Astrophysics Cambridge, MA, United States)
Lorenzini, Enrico C.
(Harvard-Smithsonian Center for Astrophysics Cambridge, MA, United States)
Gramer, Daniel J.
(Orbital Technologies Corp. Madison, WI, United States)
Hoffman, John H.
(Texas Univ. Dallas, TX, United States)
Mazzoleni, Andre P.
(North Carolina State Univ. Raleigh, NC, United States)
Date Acquired
September 7, 2013
Publication Date
April 26, 2005
Subject Category
Lunar And Planetary Science And Exploration
Meeting Information
Meeting: 41st AIAA Joint Propulsion Conference
Location: Tucson, AZ
Country: United States
Start Date: July 10, 2005
End Date: July 13, 2005
Funding Number(s)
CONTRACT_GRANT: NAS8-03041
Distribution Limits
Public
Copyright
Public Use Permitted.
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