NASA's Space Shuttle Processing Status Report

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10.06.06

Jessica Rye
Kennedy Space Center, Fla.
321-867-2468

STATUS REPORT: S-100606

NASA'S SPACE SHUTTLE PROCESSING STATUS REPORT

Note: NASA's Kennedy Space Center issues Space Shuttle Processing 
Status Reports periodically and is the source for information 
regarding processing activities associated with the vehicles and 
payloads.  If you are a member of the media and would like further 
information, visit:  
http://www.nasa.gov/centers/kennedy/news/index.html  

Mission: STS-116 - 20th International Space Station Flight (12A.1) - 
P5 Truss Segment 
Vehicle: Discovery (OV-103) 
Location: Orbiter Processing Facility Bay 3 
Launch Date: No earlier than Dec. 7, 2006 
Launch Pad: 39B 
Crew: Polansky, Oefelein, Curbeam, Higginbotham, Patrick, Fuglesang 
and Williams 
Inclination/Orbit Altitude: 51.6 degrees/122 nautical miles 

During Thursday's Program Requirements Control Board meeting, Space 
Shuttle Program managers discussed the self-imposed restriction to 
daylight launches of the first two missions following the Columbia 
accident. The Program agreed to evaluate daylight versus night 
launches on a mission by mission basis when requirements for highly 
desirable launch and ascent imagery are identified. The consensus was 
that restoring night launch capability of the shuttle does not impose 
additional risk to the safety of the vehicle and crew. It provides 
flexibility in scheduling missions to the International Space Station 
toward fulfilling the shuttle's mission to finish station 
construction within the remaining life of the shuttle fleet prior to 
the fleet's retirement in 2010. The current no earlier than launch 
date would have a launch time of 9:38 p.m.

Engineers reviewed the damage to orbiter Discovery's right-hand 
external tank door mechanism, which resulted during the process of 
reassembling the linkage following the changeout of the power drive 
unit. Replacement parts will be delivered to the bay today and are 
scheduled to be installed early next week. There is no impact to the 
overall processing schedule.

The STS-116 crew will be at Kennedy Space Center next week for the 
crew equipment interface test. A routine part of astronaut training 
and launch preparations, the test activities allow for equipment 
familiarization and inspection of the items and hardware that will be 
used during the mission.

In the Vehicle Assembly Building, solid rocket booster stacking is 
complete and technicians are working on final joint closeout. Program 
managers will hold the external tank and booster mate review on Oct. 
10, followed by the mating on Oct. 13 of the external tank, 
designated ET-123, scheduled to fly with Discovery. 

Mission: STS-117 - 21st International Space Station Flight (13A) - 
S3/S4 Truss Segment Solar Arrays 
Vehicle: Atlantis (OV-104) 
Location: Orbiter Processing Facility Bay 1 
Launch Date: No earlier than Feb. 22, 2007 
Launch Pad: 39B 
Crew: Sturckow, Archambault, Reilly, Forrester, Swanson and Olivas 
Inclination/Orbit Altitude: 51.6 degrees/122 nautical miles 

Technicians continue performing post-landing inspections on orbiter 
Atlantis and are about 85 percent complete with the review of the 
thermal protection system. During inspections, a 0.1-inch diameter 
impact was noted on Atlantis' right-hand payload bay door radiator. 
The damage has been preliminarily identified as caused by 
micrometeoroid orbital debris (MMOD), which passed through the 
radiator's face (outer) sheet, interior honeycomb structure and inner 
sheet. The MMOD did not impact the payload bay door itself. Ground 
operations personnel at Kennedy Space Center will repair the damage 
as soon as a plan is developed and approved, while ensuring the site 
is protected for analysis by orbital debris experts at Johnson Space 
Center.

This week, technicians performed the forward reaction control system 
functional test and checkout, with a similar test scheduled for the 
orbiter maneuvering system this weekend. On Oct. 1, technicians 
removed the three space shuttle main engines from the aft of the 
vehicle. Wing leading edge thermography on the reinforced 
carbon-carbon panels is complete and the chin panel, located under 
the nose cap, has been removed. 

Endeavour (OV-105)

Endeavour remains powered down in Orbiter Processing Facility bay 2 
and technicians continue preparing the vehicle for its first launch 
following an extensive modification period. Exhaust duct leak checks 
are complete on auxiliary power unit No. 1.

Work continues on the orbiter boom sensor system manipulator 
positioning mechanism. The mechanisms serve as the pedestals that 
hold the boom in place in the payload bay when it is not in use. The 
aft pedestal is installed for flight.

	
-end-



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