Aluminium alloys are used in spacecraft and aerospace industries because of their
unique properties which are lightweight and high strength. The components of aluminium
alloys used in aerospace and space environment are subjected to relative motion which results
in the tribo-phenomenon. The designer needs tribo response data for designing components
geometrical dimensions. The literature reports inadequate tribo response data, more particularly
in a vacuum environment (adverse environment). In the present investigation, experiments
were conducted using Al 6061 aluminium alloy pins with different diameters. The cylindrical
pin diameters were 2mm, 4mm and 6 mm. The cylindrical pins were slid against a hardened
En-8 steel disc. The normal pressure was maintained at 0.625 MPa and the sliding speed was
0.5 ms-1. The estimated friction coefficient from monitored frictional force and normal force
and the dependency of estimated friction coefficient on sliding distance for cylindrical pins of
different diameters were analysed
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