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The Propulsive Small Expendable Deployer System (ProSEDS)This Final Report covers the following main topics: 1) Brief Description of ProSEDS; 2) Mission Analysis; 3) Dynamics Reference Mission; 4) Dynamics Stability; 5) Deployment Control; 6) Updated System Performance; 7) Updated Mission Analysis; 8) Updated Dynamics Reference Mission; 9) Updated Deployment Control Profiles and Simulations; 10) Updated Reference Mission; 11) Evaluation of Power Delivered by the Tether; 12) Deployment Control Profile Ref. #78 and Simulations; 13) Kalman Filters for Mission Estimation; 14) Analysis/Estimation of Deployment Flight Data; 15) Comparison of ED Tethers and Electrical Thrusters; 16) Dynamics Analysis for Mission Starting at a Lower Altitude; 17) Deployment Performance at a Lower Altitude; 18) Satellite Orbit after a Tether Cut; 19) Deployment with Shorter Dyneema Tether Length; 20) Interactive Software for ED Tethers.
Document ID
20040014957
Acquisition Source
Marshall Space Flight Center
Document Type
Contractor or Grantee Report
Authors
Lorenzini, Enrico C.
(Smithsonian Astrophysical Observatory Cambridge, MA, United States)
Cosmo, Mario L.
(Smithsonian Astrophysical Observatory Cambridge, MA, United States)
Estes, Robert D.
(Smithsonian Astrophysical Observatory Cambridge, MA, United States)
Sanmartin, Juan
(Smithsonian Astrophysical Observatory Cambridge, MA, United States)
Pelaez, Jesus
(Smithsonian Astrophysical Observatory Cambridge, MA, United States)
Ruiz, Manuel
(Smithsonian Astrophysical Observatory Cambridge, MA, United States)
Date Acquired
September 7, 2013
Publication Date
December 1, 2003
Subject Category
Spacecraft Design, Testing And Performance
Funding Number(s)
CONTRACT_GRANT: NAG8-1605
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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