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Dynamics Simulation Model for Space TethersThis document describes the development of an accurate model for the dynamics of the Momentum Exchange Electrodynamic Reboost (MXER) system. The MXER is a rotating tether about 100-km long in elliptical Earth orbit designed to catch payloads in low Earth orbit and throw them to geosynchronous orbit or to Earth escape. To ensure successful rendezvous between the MXER tip catcher and a payload, a high-fidelity model of the system dynamics is required. The model developed here quantifies the major environmental perturbations, and can predict the MXER tip position to within meters over one orbit.
Document ID
20060051891
Acquisition Source
Marshall Space Flight Center
Document Type
Contractor Report (CR)
Authors
Levin, E. M.
(Star Technology and Research, Inc. Mount Pleasant, SC, United States)
Pearson, J.
(Star Technology and Research, Inc. Mount Pleasant, SC, United States)
Oldson, J. C.
(Star Technology and Research, Inc. Mount Pleasant, SC, United States)
Date Acquired
September 7, 2013
Publication Date
June 1, 2006
Subject Category
Astrodynamics
Report/Patent Number
NASA/CR-2006-214432
M-1164
Report Number: NASA/CR-2006-214432
Report Number: M-1164
Funding Number(s)
CONTRACT_GRANT: NNM04AB51C
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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