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Tethers open new space optionsSeveral examples of possible applications of the tethering concept in space are examined. In particular, attention is given to a practical design of a 500-kg satellite system to be tethered at a distance of 100 km from the Space Shuttle. The satellite body has the form of a sphere, aerodynamically stabilized and fitted with a dockline adapter that mates with a capture mechanism at the tip of an extendable boom; the tether is a very flexible synthetic line 1-2 mm in diameter. Other applications include a wholly passive stable platform created by tethering two rows of empty Shuttle External Tanks or similar masses 10-20 km apart, a remote docking port for a space station, and constellations of space objects, with tethers used to tie them together and constrain their relative motions.
Document ID
19830047474
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Bekey, I.
(NASA Office of Space Flight Washington, DC, United States)
Date Acquired
August 11, 2013
Publication Date
April 1, 1983
Publication Information
Publication: Astronautics and Aeronautics
Volume: 21
Subject Category
Launch Vehicles And Space Vehicles
Accession Number
83A28692
Distribution Limits
Public
Copyright
Other

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