| Total EVAs: | 6 | ||
| Total EVA time: | 39h 11m |
| No. | Date | Together with | Time | Main tasks and notes |
| 1 | 10.12.2001 | L. Godwin | 4h 12m |
Adding insulation blankets around two critical
solar array drive, but they were unable to tighten up a solar array support
truss |
| 2 | 28.10.2007 | S. Parazynski | 6h 33m |
Disconnect Z1 to P6 truss cables and unbolt P6;
outfit outside Node 2 with handrails, worksite interface fixtures, gap spanners
and install thermal covers, remote Node 2 berthing mechanism restraints;
install grapple fixture on Node 2; configure squib firing unit on S1 truss for
deploying radiators. |
| 3 | 20.11.2007 | P. Whitson | 7h 16m |
Complete the exterior hookup of Harmony. Much of
the spacewalk included the moving of a 300-pound, 18.5-foot fluid tray from its
temporary location at the center of the station's main truss to
Harmony. |
| 4 | 24.11.2007 | P. Whitson | 7h 04m |
Complete the exterior hookup of Harmony. Much of
the spacewalk included the moving of another 300-pound, 18.5-foot fluid tray
from its temporary location at the center of the station's main truss to
Harmony. |
| 5 | 18.12.2007 | P. Whitson | 6h 56m |
Examination of the starboard Solar Alpha Rotary
Joint (SARJ) and return a trundle assembly to the station's
interior. |
| 6 | 30.01.2008 | P. Whitson | 7h 10m |
Replacing a motor with electrical failures, the
Bearing Motor Roll Ring Module (BMRRM), called the 'broom". The motor drives
the starboard solar wings as they tilt along their axis to follow the sun for
optimal power generation as the station orbits the Earth. The second main goal
of the spacewalk was inspection of the starboard Solar Alpha Rotary Joint (SARJ). That device causes the starboard solar wings to
rotate in a paddlewheel-like motion to keep the arrays pointed toward the
sun. |