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In-orbit experimentation with the Small Expendable-Tether Deployment SystemThe Small Expendable-Tether Deployment System (SEDS) is a light-weight deployer capable of deploying instrumented packages and other tethered payloads up to a distance of 20 km. The system is simple and inexpensive because it does not retrieve the tethered payloads. The deployer is attached to the second stage of a Delta II which acts as a stabilized platform for the deployment of tethered payloads. SEDS is particularly suitable for complementing the Tethered Satellite missions by providing a flexible system for experimenting with the tether-in-space technology. SEDS can also provide a convenient way for testing instruments and/or procedures which require the use of long tethers.
Document ID
19910029140
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lorenzini, Enrico C.
(Harvard-Smithsonian Center for Astrophysics Cambridge, MA, United States)
Carroll, Joseph A.
(Tether Applications San Diego, CA, United States)
Date Acquired
August 14, 2013
Publication Date
October 1, 1990
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
IAF PAPER 90-048
Accession Number
91A13763
Distribution Limits
Public
Copyright
Other

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