NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Metering Wheel-Wire Track Wire Boom Deployment MechanismThe NASA MMS Spin Plane Double Probe (SDP) Deployer utilizes a helical path, rotating Metering Wheel and a spring loaded Wire "Holding" Track to pay out a "fixed end" 57 meter x 1.5 mm diameter Wire Boom stored between concentric storage cylinders. Unlike rotating spool type storage devices, the storage cylinders remain stationary, and the boom wire is uncoiled along the length of the cylinder via the rotation of the Metering Wheel. This uncoiling action avoids the need for slip-ring contacts since the ends of the wire can remain stationary. Conventional fixed electrical connectors (Micro-D type) are used to terminate to operational electronics.
Document ID
20150004044
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Granoff, Mark S.
(New Hampshire Univ. Durham, NH, United States)
Date Acquired
April 2, 2015
Publication Date
May 1, 2014
Publication Information
Publication: The 42nd Aerospace Mechanism Symposium
Subject Category
Mechanical Engineering
Meeting Information
Meeting: Aerospace Mechanisms Symposium
Location: Greenbelt, MD
Country: United States
Start Date: May 14, 2014
End Date: May 16, 2014
Sponsors: NASA Goddard Space Flight Center
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available