Computer Science – Robotics
Scientific paper
Oct 1992
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1992stin...9312682r&link_type=abstract
Unknown
Computer Science
Robotics
Gas Tungsten Arc Welding, Graphite-Epoxy Composites, Large Space Structures, Orbital Assembly, Robotics, Trusses, Welded Joints, Aerobraking, Aluminum Alloys, Computer Programs
Scientific paper
A preliminary design for a weldable truss joint for on-orbit assembly of large space structures is described. The joint was designed for ease of assembly, for structural efficiency, and to allow passage of fluid (for active cooling or other purposes) along the member through the joint. The truss members were assumed to consist of graphite/epoxy tubes to which were bonded 2219-T87 aluminum alloy end fittings for welding on-orbit to truss nodes of the same alloy. A modified form of gas tungsten arc welding was assumed to be the welding process. The joint was designed to withstand the thermal and structural loading associated with a 120-ft diameter tetrahedral truss intended as an aerobrake for a mission to Mars.
Rule William K.
Thomas F. P.
No associations
LandOfFree
Design of a welded joint for robotic, on-orbit assembly of space trusses does not yet have a rating. At this time, there are no reviews or comments for this scientific paper.
If you have personal experience with Design of a welded joint for robotic, on-orbit assembly of space trusses, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Design of a welded joint for robotic, on-orbit assembly of space trusses will most certainly appreciate the feedback.
Profile ID: LFWR-SCP-O-1871847