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With the landing of ''Discovery'' after the [[STS-131]] mission, ''Leonardo'' was transferred back to the Space Station Processing Facility at Kennedy Space Center. ''Leonardo'' began receiving modifications and reconfigurations immediately to convert it for permanent attachment to the space station and to facilitate on-orbit maintenance.<ref>{{cite web|url=http://www.nasaspaceflight.com/2010/10/pmm-leonardo-final-permanent-us-module-iss/|title=PMM Leonardo: The Final Permanent U.S. Module for the ISS
 
With the landing of ''Discovery'' after the [[STS-131]] mission, ''Leonardo'' was transferred back to the Space Station Processing Facility at Kennedy Space Center. ''Leonardo'' began receiving modifications and reconfigurations immediately to convert it for permanent attachment to the space station and to facilitate on-orbit maintenance.<ref>{{cite web|url=http://www.nasaspaceflight.com/2010/10/pmm-leonardo-final-permanent-us-module-iss/|title=PMM Leonardo: The Final Permanent U.S. Module for the ISS
|author=Chris Gebhardt|date=6 October 2010|accessdate=15 November 2010|publisher=NASAspaceflight.com}}</ref> Some equipment was removed to reduce the overall weight of ''Leonardo''. These removals resulted in a net weight loss of {{convert|178.1|lbs|kg|abbr=on}}. Additional modifications to ''Leonardo'' included the installation of upgraded [[multi-layer insulation]] (MLI) and [[Whipple shield|Micro Meteoroid Orbital Debris]] (MMOD) shielding to increase the ability of the PMM to handle potential impacts of [[micrometeoroid]]s or [[orbital debris]]; a Planar Reflector was installed at the request of the Japanese Space Agency (JAXA).
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|author=Chris Gebhardt|date=6 October 2010|accessdate=15 November 2010|publisher=NASAspaceflight.com}}</ref> Some equipment was removed to reduce the overall weight of ''Leonardo''. These removals resulted in a net weight loss of {{convert|178.1|lbs|kg|abbr=on}}. Additional modifications to ''Leonardo'' included the installation of upgraded [[multi-layer insulation]] (MLI) and [[Whipple shield|Micro Meteoroid Orbital Debris]] (MMOD) shielding to increase the ability of the PMM to handle potential impacts of [[micrometeoroid]]s or [[orbital debris]]; a Planar Reflector was installed at the request of the [[JAXA|Japanese Space Agency]] (JAXA).
   
 
Following berthing to the space station, the contents of ''Leonardo'' were emptied and moved to appropriate locations on the ISS. Once JAXA's [[Kounotori 2]] (HTV-2) arrived in February 2011, ''Leonardo'''s now-unnecessary launch hardware was transferred to HTV2 for ultimate destruction in Earth's atmosphere.
 
Following berthing to the space station, the contents of ''Leonardo'' were emptied and moved to appropriate locations on the ISS. Once JAXA's [[Kounotori 2]] (HTV-2) arrived in February 2011, ''Leonardo'''s now-unnecessary launch hardware was transferred to HTV2 for ultimate destruction in Earth's atmosphere.
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File:STS-133 crew arrival.jpg|The crew pose for a photo at the KSC (including Bowen).
 
File:STS-133 crew arrival.jpg|The crew pose for a photo at the KSC (including Bowen).
 
File:Sts133 mission poster.jpg|Mission poster (with Kopra instead of Bowen).
 
File:Sts133 mission poster.jpg|Mission poster (with Kopra instead of Bowen).
File:President Obama Meets With STS-133 Crew.jpg|Lindsey, far left, presents a montage to Barack Obama as crew members Barratt, Boe, Stott and Bowen look on.
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File:President Obama Meets With STS-133 Crew.jpg|Lindsey, far left, presents a montage to [[Barack Obama]] as crew members Barratt, Boe, Stott and Bowen look on.
 
</gallery>
 
</gallery>
   
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===Orbital Maneuvering System vapor leak===
 
===Orbital Maneuvering System vapor leak===
On 14 October 2010, engineers at the launch pad first discovered a small leak in a propellant line for ''Discovery''<nowiki>'</nowiki>s orbital maneuvering system (OMS) engines. The leak was detected after they noticed a fishy smell coming from the aft of the shuttle, thought of as a sign of fuel vapor in the air.<ref name="vapor leak">{{cite web|url=http://www.nasaspaceflight.com/2010/10/sts-133-tcdt-completed-troubleshooting-leaky-flight-cap/|title=STS-133: TCDT completed – Engineers troubleshooting leaky flight cap|author=Chris Bergin|publisher=NASAspaceflight.com|date=15 October 2010|accessdate=19 October 2010}}</ref> Upon inspection, the leak was found at a flange located at the interface where two propellant lines met in ''Discovery''<nowiki>'</nowiki>s aft compartment. The line carried [[monomethyl hydrazine]] (MMH) propellant, one of two chemicals (the other is an oxidizer, nitrogen tetroxide) used to ignite the OMS engines. Engineers replaced an Air Half Coupling (AHC) flight cap. However, the new cap failed to solve the problem since vapor checks still showed signs of a leak. An aspirator was activated to collect the vapor at the leak-site allowing work to continue in other locations around the aft segment of ''Discovery''.
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On 14 October 2010, engineers at the launch pad first discovered a small leak in a propellant line for ''Discovery''<nowiki>'</nowiki>s orbital maneuvering system (OMS) engines. The leak was detected after they noticed a fishy smell coming from the aft of the shuttle, thought of as a sign of fuel vapor in the air.<ref name="vapor leak">{{cite web|url=http://www.nasaspaceflight.com/2010/10/sts-133-tcdt-completed-troubleshooting-leaky-flight-cap/|title=STS-133: TCDT completed – Engineers troubleshooting leaky flight cap|author=Chris Bergin|publisher=NASAspaceflight.com|date=15 October 2010|accessdate=19 October 2010}}</ref> Upon inspection, the leak was found at a flange located at the interface where two propellant lines met in ''Discovery''<nowiki>'</nowiki>s aft compartment. The line carried [[monomethyl hydrazine]] (MMH) propellant, one of two chemicals (the other is an oxidizer, [[nitrogen tetroxide]]) used to ignite the OMS engines. Engineers replaced an Air Half Coupling (AHC) flight cap. However, the new cap failed to solve the problem since vapor checks still showed signs of a leak. An aspirator was activated to collect the vapor at the leak-site allowing work to continue in other locations around the aft segment of ''Discovery''.
   
 
It was believed that the leak was in the crossfeed flange area – a problem with associated seals. On 18 October 2010, after an afternoon review, engineers were asked to double-check the torque on six bolts around the suspected leaky flange fitting and tighten if necessary.<ref>{{cite web|url=http://www.spaceflightnow.com/shuttle/sts133/101018leak/|title=Technicians working on tiny fuel leak in Discovery pod
 
It was believed that the leak was in the crossfeed flange area – a problem with associated seals. On 18 October 2010, after an afternoon review, engineers were asked to double-check the torque on six bolts around the suspected leaky flange fitting and tighten if necessary.<ref>{{cite web|url=http://www.spaceflightnow.com/shuttle/sts133/101018leak/|title=Technicians working on tiny fuel leak in Discovery pod
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===Johannes Kepler ATV rescheduled===
 
===Johannes Kepler ATV rescheduled===
The launch date of 24 February 2011 was officially set after the Flight Readiness Review meeting on 18 February 2011. Reviews of previous problems, including the GUP vent line connection, external tank foam and external tank stringer cracks, were found to be positive. Additionally, flight rules which required a 72-hour separation between dockings at the International Space Station threatened to delay the launch by at least a day due to the delayed launch of the ESA's unmanned [[Johannes Kepler ATV]] supply craft. Managers instead decided to press ahead with the countdown allowing for a possible standdown; had docking issues arisen with the ATV, STS-133 would have stood down for 48 hours.<ref>{{cite news|last=Bergin|first=Chris|title=STS-133: FRR approves Discovery's launch for next Thursday|url=http://www.nasaspaceflight.com/2011/02/sts-133-frr-approves-launch-for-next-thursday/|newspaper=Spaceflight Now|date=18 February 2011}}</ref> The Kepler ATV docked successfully at 10:59 UTC, 24 February 2011.<ref name=nasatv>[http://www.nasa.gov/multimedia/nasatv/ NASA.gov/multimedia/nasatv/: ''per NASA Live TV broadcast'']</ref>
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The launch date of 24 February 2011 was officially set after the Flight Readiness Review meeting on 18 February 2011. Reviews of previous problems, including the GUP vent line connection, external tank foam and external tank stringer cracks, were found to be positive. Additionally, flight rules which required a 72-hour separation between dockings at the International Space Station threatened to delay the launch by at least a day due to the delayed launch of the [[ESA]]'s unmanned [[Johannes Kepler ATV]] supply craft. Managers instead decided to press ahead with the countdown allowing for a possible standdown; had docking issues arisen with the ATV, STS-133 would have stood down for 48 hours.<ref>{{cite news|last=Bergin|first=Chris|title=STS-133: FRR approves Discovery's launch for next Thursday|url=http://www.nasaspaceflight.com/2011/02/sts-133-frr-approves-launch-for-next-thursday/|newspaper=Spaceflight Now|date=18 February 2011}}</ref> The Kepler ATV docked successfully at 10:59 UTC, 24 February 2011.<ref name=nasatv>[http://www.nasa.gov/multimedia/nasatv/ NASA.gov/multimedia/nasatv/: ''per NASA Live TV broadcast'']</ref>
   
 
==Launch attempts==
 
==Launch attempts==
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| Day 8
 
| Day 8
 
| "[[City of Blinding Lights]]"
 
| "[[City of Blinding Lights]]"
| U2
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| [[U2]]
 
| [[STS-133#Crew|STS-133 Crew]]
 
| [[STS-133#Crew|STS-133 Crew]]
 
| [http://ia700406.us.archive.org/13/items/STS-133/03-03-11_STS-133_FD8_Crew_Wakeup.wav WAV], [http://ia700406.us.archive.org/13/items/STS-133/03-03-11_STS-133_FD8_Crew_Wakeup-01.mp3 MP3]
 
| [http://ia700406.us.archive.org/13/items/STS-133/03-03-11_STS-133_FD8_Crew_Wakeup.wav WAV], [http://ia700406.us.archive.org/13/items/STS-133/03-03-11_STS-133_FD8_Crew_Wakeup-01.mp3 MP3]
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{{Space Shuttle Discovery}}
 
{{Space Shuttle Discovery}}
 
{{Manned ISS flight}}
 
{{Manned ISS flight}}
 
{{Wikipedia|STS-133}}
 
   
 
{{DEFAULTSORT:Sts-133}}
 
{{DEFAULTSORT:Sts-133}}
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