NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Orbital Winch for High-Strength, Space-Survivable TethersAn Orbital Winch mechanism enables high-load, multi-line tethers to be deployed and retracted without rotating the spool on which the tether is wound. To minimize damage to the tether and the wound package during retraction or deployment under load, it can incorporate a Tension Management Module that reduces the infeed tension by a factor of 15 through the use of a powered capstan with guide rollers. This design eliminates the need for rotating high-voltage electrical connections in tether systems that use propellantless electro-dynamic propulsion. It can also eliminate the need for rotating optical connections in applications where the tether contains optical fibers. This winch design was developed to deploy a 15-km-long, 15-kg high-strength Hoytether structure incorporating conductive wires as part of the MXER-1 demonstration mission concept. Two slewing rings that orbit around the tether spool, combined with translation of one of the slewing rings back and forth along the spool axis to traverse the wind point, enables the winch to wind the tether. Variations of the traverse motion of the slewing ring can accomplish level winds and conical pirn winds. By removing the non-traversing slewing ring, and adding an actuated guide arm, the winch can manage rapid, low-drag deployment of a tether off the end of a pirn-wound spool, followed by controlled retraction and rewinding, in a manner very similar to a spin-casting reel. The winch requires at least two motor driver controller units to coordinate the action of two stepper motors to accomplish tether deployment or retraction.
Document ID
20100023367
Acquisition Source
Marshall Space Flight Center
Document Type
Other - NASA Tech Brief
Authors
Hoyt, Robert
(Tethers Unltd., Inc. United States)
Barnes, Ian
(Tethers Unltd., Inc. United States)
Slostad, Jeffrey
(Tethers Unltd., Inc. United States)
Frank, Scott
(Tethers Unltd., Inc. United States)
Date Acquired
August 24, 2013
Publication Date
June 1, 2010
Publication Information
Publication: NASA Tech Briefs, June 2010
Subject Category
Man/System Technology And Life Support
Report/Patent Number
MFS-32589-1
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available