NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Due to the lapse in federal government funding, NASA is not updating this website. We sincerely regret this inconvenience.

Back to Results
System requirements and design features of Space Station Remote Manipulator System mechanismsThe Space Station Remote Manipulator System (SSRMS) is a long robotic arm for handling large objects/payloads on the International Space Station Freedom. The mechanical components of the SSRMS include seven joints, two latching end effectors (LEEs), and two boom assemblies. The joints and LEEs are complex aerospace mechanisms. The system requirements and design features of these mechanisms are presented. All seven joints of the SSRMS have identical functional performance. The two LEES are identical. This feature allows either end of the SSRMS to be used as tip or base. As compared to the end effector of the Shuttle Remote Manipulator System, the LEE has a latch and umbilical mechanism in addition to the snare and rigidize mechanisms. The latches increase the interface preload and allow large payloads (up to 116,000 Kg) to be handled. The umbilical connectors provide power, data, and video signal transfer capability to/from the SSRMS.
Document ID
19910015291
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kumar, Rajnish
(Spar Aerospace Ltd. Toronto Ontario, Canada)
Hayes, Robert
(Spar Aerospace Ltd. Toronto Ontario, Canada)
Date Acquired
September 6, 2013
Publication Date
May 1, 1991
Publication Information
Publication: JPL, The 25th Aerospace Mechanisms Symposium
Subject Category
Mechanical Engineering
Accession Number
91N24605
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available