 Canadarm2 grapples the exposed facility ofKibō, prior to its installation on the ISS | |
| Names | Space Transportation System-127 |
|---|---|
| Mission type | ISS assembly |
| Operator | NASA |
| COSPAR ID | 2009-038A |
| SATCATno. | 35633 |
| Mission duration | 15 days, 16 hours, 44 minutes, 58 seconds |
| Distance travelled | 10,537,748 kilometres (6,547,853 mi) |
| Orbits completed | 248[1] |
| Spacecraft properties | |
| Spacecraft | Space Shuttle Endeavour |
| Crew | |
| Crew size | 7 |
| Members | |
| Launching | |
| Landing | |
| Start of mission | |
| Launch date | July 15, 2009, 22:03 (2009-07-15UTC22:03Z) UTC |
| Launch site | Kennedy,LC-39A |
| End of mission | |
| Landing date | July 31, 2009, 14:48 (2009-07-31UTC14:49Z) UTC |
| Landing site | Kennedy,SLF Runway 15 |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Low Earth |
| Perigee altitude | 344 kilometres (214 mi)[2] |
| Apogee altitude | 351 kilometres (218 mi)[2] |
| Inclination | 51.6 degrees[1][2] |
| Period | 91.48 minutes[2] |
| Epoch | July 18, 2009[2] |
| Docking withISS | |
| Docking port | PMA-2 (Harmony forward) |
| Docking date | July 17, 2009 17:47 UTC |
| Undocking date | July 28, 2009 17:26 UTC |
| Time docked | 10 days, 23 hours, 41 minutes |
  From left to right: Wolf, Cassidy, Hurley, Payette, Polansky, Marshburn, and Kopra | |
STS-127 (ISS assembly flight2J/A) was aNASASpace Shuttle mission to theInternational Space Station (ISS).[1] It was the twenty-third flight ofSpace Shuttle Endeavour. The primary purpose of the STS-127 mission was to deliver and install the final two components of theJapanese Experiment Module: theExposed Facility (JEM EF), and theExposed Section of the Experiment Logistics Module (ELM-ES).[3][NASA 1] WhenEndeavour docked with the ISS on this mission in July 2009, it set a record for the most humans in space at the same time in the same vehicle, the first time thirteen people have been at the station at the same time.[4] Together they represented allISS program partners[5] and tied the general record of thirteen people in space with the first such occurrence of 1995.[6]
The first launch attempt, on June 13, 2009, was scrubbed due to a gaseous hydrogen leak observed during tanking.[7][8] The Ground Umbilical Carrier Plate (GUCP) on the external fuel tank experienced a potentially hazardous hydrogen gas leak similar to the fault that delayed theSpace Shuttle Discovery missionSTS-119 in March 2009. Since a launch date of June 18, 2009, would have conflicted with the launch of theLunar Reconnaissance Orbiter (LRO)/Lunar Crater Observation and Sensing Satellite (LCROSS), NASA managers discussed the scheduling conflict with both the Lunar Reconnaissance Orbiter project and theAir Force Eastern Range, which provides tracking support for rockets launched from Florida.[9][10] A decision was made to allow the shuttle to attempt a second launch on June 17, 2009, allowing LRO to launch on June 18, 2009.[8]
The second launch attempt on June 17, 2009, was also scrubbed due to hydrogen leak issues seen from theGround Umbilical Carrier Plate.[11] Due to conflicts with the launch of the LRO, and due to abeta angle constraint, the next available launch opportunity was scheduled for July 11, 2009.[NASA 2][12] A successful tanking test for leak checks was performed on July 1, 2009, with modified GUCP seals allowing launch preparations to proceed as scheduled.[13] Because of lightning strikes near the launch pad during the evening of July 10, 2009, NASA scrubbed the launch for the third time and rescheduled for July 12, 2009.[14] Due to aReturn To Launch Site (RTLS) weather violation, NASA scrubbed the launch for the fourth time on the evening of July 12, 2009.
STS-127's fifth launch attempt, on July 13, 2009, was also scrubbed due toanvil clouds andlightning within 10 nautical miles (19 km) of the launch site, which violated launch safety rules. STS-127 finally launched successfully on its sixth launch attempt, on July 15, 2009, at 18:03 EDT. Pieces of foam were observed falling off of the External Tank during the ascent, the same occurrence that had led to theloss ofColumbia in 2003. However,Endeavour received only minor scuffs to its heat shield, the damage not enough to cause concern over reentry.[15] The shuttle landed atKennedy Space Center 16 days later at 10:48 EDT on July 31, 2009.
| Position[1][NASA 1][NASA 3] | Launching Astronaut | Landing Astronaut |
|---|---|---|
| Commander |  Mark L. PolanskyThird and last spaceflight | |
| Pilot | Douglas G. Hurley First spaceflight | |
| Mission Specialist 1 | Christopher J. Cassidy First spaceflight | |
| Mission Specialist 2 Flight Engineer |  Julie Payette,CSASecond and last spaceflight | |
| Mission Specialist 3 | Thomas H. Marshburn First spaceflight | |
| Mission Specialist 4 | David Wolf Fourth and last spaceflight | |
| Mission Specialist 5 | Timothy Kopra Expedition 20 First spaceflight |  Koichi Wakata,JAXAExpedition 20 Third spaceflight |
| STS-127 marked the first time that two Canadian astronauts,Robert Thirsk and Julie Payette, were in space at the same time. Christopher Cassidy was the 500thperson to fly in space.[16] | ||
| Seat[17] | Launch | Landing |  Seats 1–4 are on the flight deck. Seats 5–7 are on the mid-deck. |
|---|---|---|---|
| 1 | Polansky | ||
| 2 | Hurley | ||
| 3 | Cassidy | Wolf | |
| 4 | Payette | ||
| 5 | Wolf | Cassidy | |
| 6 | Marshburn | ||
| 7 | Kopra | Wakata | |
Endeavour carried a wide variety of equipment and cargo in the payload bay, with the largest item being theKibō Japanese Experiment Module Exposed Facility (JEM EF), and theKibō Japanese Experiment Logistics Module – Exposed Section (ELM-ES).[NASA 1] The exposed facility is a part ofKibō that will allow astronauts to perform science experiments that are exposed to the vacuum of space. The exposed section is similar to the logistics module on theKibō laboratory, but is not pressurized.[NASA 1] Once its payloads were transferred to the JEM EF, the ELM-ES was returned to the payload bay.
Also inside the payload bay was anIntegrated Cargo Carrier-Vertical Light Deployable (ICC-VLD), containing a variety of equipment and spare components for the station. The carrier contained six new batteries for installation on theP6 truss, that was installed during two of the mission's spacewalks, as well as a spare space-to-ground antenna and a spare linear drive unit and pump module which was stored on an external stowage platform on the station's truss during one of the spacewalks.[NASA 1]
Two satellites were also carried by the orbiter, for deployment when the mission ended. The Dual Autonomous Global Positioning System On-Orbit Navigator Satellite, called DRAGONSAT, gathers data on autonomous spacecraft rendezvous and docking capabilities, and consists of twopicosatellites, the AggieSat2, and PARADIGM (BEVO-1), which acquireGPS data from a device at NASA and send it to ground stations atTexas A&M University and theUniversity of Texas at Austin.[NASA 1][NASA 4] After release, the two picosatellites remained attached for two orbits to collect GPS data, and separated during the third orbit.[NASA 1]
A second satellite, the Atmospheric Neutral Density Experiment (ANDE-2), is part of aUnited States Department of Defense project flown by theNaval Research Laboratory to provide high-quality satellites, and will measure the density and composition of thelow Earth orbitatmosphere while being tracked from the ground, to better predict the movement and decay of objects in orbit.[NASA 1][NASA 5] ANDE-2 consists of two sphericalmicrosatellites, ANDE Active spacecraft (Castor) and the ANDE Passive spacecraft (Pollux), and will be tracked by the International Laser Ranging Service (ILRS) network as well as theSpace Surveillance Network (SSN).[NASA 1][NASA 5] One of the satellites, Pollux, is runningArduino libraries, with its payload programmed and built by students.
A set of experiments to be deployed on the ISS were carried by STS-127, including Dosimetry for Biological Experiments in Space (ESA), Validation of Procedures for Monitoring Crew Member Immune Function, the student-made Image Reversal in Space (CSA/ISU), Nutritional Status Assessment (NASA), NASA Biological Specimen Repository and Tomatosphere-II (CSA).[NASA 1]
The STS-127 Official Flight Kit (OFK) included water samples from each of the fiveGreat Lakes, a resin statue of a water droplet for theOne Drop Foundation, and a copy ofBeethoven'sFifth Symphony for theMontreal Symphony Orchestra, among other mementos.[18]
The docking module was also mounted with the DragonEye3D Flash LIDAR ranging system manufactured byAdvanced Scientific Concepts, Inc. The module was launched to test the docking system which will be used by the commercialSpaceX Dragon re-usable cargo carrier to send supplies to the ISS during the post-shuttle era. The Dragon spacecraft made its successful maiden flight in December 2010.[19]
| Location | Cargo | Mass |
|---|---|---|
| Bays 1–2 | Orbiter Docking System EMU 3003 / EMU 3018 SpaceX DragonEyeLIDAR | 1,800 kilograms (4,000 lb) ~260 kilograms (570 lb) |
| Bay 3P | Shuttle Power Distribution Unit (SPDU) | ~17 kilograms (37 lb) |
| Bay 3S | APC/SSPL Dragonsat | 51 kilograms (112 lb) 6 k |
| Bays 4–7 | Kibō JEM Exposed Facility | 3,820 kilograms (8,420 lb) |
| Bay 5P | APC/ECSH | ~33 kilograms (73 lb) |
| Bay 5S | APC/PPSU | 20 kilograms (44 lb) |
| Bay 6S | APC/PPSU | 20 kilograms (44 lb) |
| Bays 8–9 | Kibō ELM Exposed Section | 2,453 kilograms (5,408 lb) |
| Bay 11 | ICC-VLD | 3,946 kilograms (8,699 lb) |
| Bay 13P | APC/ECSH | ~33 kilograms (73 lb) |
| Bay 13S | SPA/CAPE/ANDE-2 ICU container ANDE Active satellite ANDE Passive satellite | 265 kilograms (584 lb) 54 kilograms (119 lb) 50 kilograms (110 lb) 25 kilograms (55 lb) |
| Starboard Sill | Orbiter Boom Sensor System | ~382 kilograms (842 lb) |
| Port Sill | Canadarm | 410 kilograms (900 lb) |
| Total: | 13,645 kilograms (30,082 lb) |
The mission marked:[1]
Endeavour served as theSTS-400rescue vehicle forSTS-125, and was prepared for a possible liftoff fromLaunch Pad 39B on May 15, 2009, four days after the launch of STS-125.[NASA 6][NASA 7] AfterAtlantis performed the late inspection and was cleared for re-entry,Endeavour was officially released from stand-by status on May 21, 2009, and preparations for STS-127 were initiated.[20]
Endeavour moved from Launch Pad 39B to 39A on May 31, 2009, in preparation for STS-127.[21][NASA 8] The crew of STS-127 arrived atKennedy Space Center on June 2, 2009, for theTerminal Countdown Demonstration Test (TCDT) that concluded with a full launch dress rehearsal.[NASA 8][22][23] The Flight Readiness Review (FRR), a meeting during which NASA managers assess mission preparations and officially set the launch date, concluded on June 3, 2009.[NASA 9] For the first time, live status updates about the FRR were published periodically during the meeting via NASA's Twitter stream.[NASA 9]
The launch countdown began June 10, 2009, but on June 13, 2009, as tanking was underway, a gaseous hydrogen leak on a vent line near the Ground Umbilical Carrier Plate was observed, and the June 13, 2009, launch was scrubbed at 00:26 EDT. As liquid hydrogen fuel is pumped in, some of it boils off as the extremely cold liquid enters the warm external tank. The vent line valve controls the resulting buildup of gas pressure by allowing excess gas to escape into a ground-side vent line, which leads to aflare stack at a safe distance away from the pad. A similar leak situation was seen during the first launch attempt ofSTS-119. NASA managers met on June 14, 2009, and June 15, 2009, and evaluated the leak, discussed steps that had to be taken, and set a new launch date of June 17, 2009, at 05:40 EDT.[7][8]
A second launch attempt was made on June 17, 2009, for which NASA moved the planned launch of theLunar Reconnaissance Orbiter to a new date. On June 17, 2009, loading of the shuttle's external tank with liquid hydrogen and liquid oxygen was delayed three hours due to poor weather around the launch site, but tanking began once the weather cleared. Approximately two hours after tanking began, engineers saw leak indications in the GUCP similar to those seen during the first launch attempt. The launch was officially scrubbed at 01:55 EDT.[11]
Following the launch scrub, Chairman of NASA's Mission Management TeamLeRoy Cain noted that engineers would work to understand the hydrogen leak issue and come up with a solution to the problem. Cain said managers were hopeful that the issue could be resolved in time for the next available launch opportunity on July 11, 2009.[24] Due to the delay of STS-127, managers noted that it was likely that the launch ofSTS-128 on August 7, 2009, would be pushed back slightly.[24]
On July 1, 2009, the shuttle managers conducted a new series of tanking tests to confirm a hypothesis that a misaligned vent port housing was the root cause of the leaks. The existing rigid seal was replaced with a flexible one in the hope that it would maintain a tight fix even under the cryogenic conditions that seem to cause the leak. The test was declared a success with no leaks detected on the GUCP. The mission was announced to be targeting a July 11, 2009, launch.[25][26] On the evening of July 10, 2009, the launch pad region was hit by eleven strikes of lightning, which pushed back the July 11, 2009, launch time by at least 24 hours. Two of the strikes were strong enough to trigger an evaluation by NASA engineers. The inspections revealed that no damage had been done to the Space Shuttle.[NASA 10]
NASA scrubbedEndeavour' July 12, 2009, launch attempt atT-minus 9 minutes and holding due to Cumulus clouds and lightning near the launch pad. During the final Go/No-Go polls, Mission Control in Houston declared a "No-Go" due to unacceptable weather forecast for a possible Return-To-Launch-Site (RTLS) abort, and planned for emergency scenarios when one or more engines shut down early leaving insufficient energy to reach the Transatlantic Abort Landing (TAL) sites. Similarly, during the July 13, 2009, attempt, RTLS weather was also "no go." Meanwhile, shuttle weather officer Kathy Winters informed the launch director,Peter Nickolenko, that the launch pad weather had changed to RED as the Phase-1 Lightning warning was issued for theKennedy Space Center. The launch was scrubbed atT-minus 9 minutes and holding and was quickly reset for July 15, 2009 (a 48 hours scrub turn around) due to weather concerns on July 14, 2009, and the desire to replace the Tyvek covers over the forward Reaction Control System thrusters.[NASA 11]
| Attempt | Planned | Result | Turnaround | Reason | Decision point | Weather go (%) | Notes |
|---|---|---|---|---|---|---|---|
| 1 | 13 Jun 2009, 7:17:19 am | Scrubbed | — | Technical | 13 Jun 2009, 12:26 am | 90%[27] | gaseous hydrogen leak on a vent line near the Ground Umbilical Carrier Plate[7] |
| 2 | 17 Jun 2009, 5:40:52 am | Scrubbed | 3 days 22 hours 24 minutes | Technical | 17 Jun 2009, 1:55 am | 80%[28] | leak persisted[11] |
| 3 | 11 Jul 2009, 7:39:38 pm | Scrubbed | 24 days 13 hours 59 minutes | Weather | 40%[29] | lightning strikes to launch pad[25] | |
| 4 | 12 Jul 2009, 7:13:55 pm | Scrubbed | 0 days 23 hours 34 minutes | Weather | 12 Jul 2009, 7:00 pm (T−00:09:00 hold) | 70%[30] | RTLS concerns, cumulus clouds and lightning near launch pad[NASA 10] |
| 5 | 13 Jul 2009, 6:51:24 pm | Scrubbed | 0 days 23 hours 37 minutes | Weather | 13 Jul 2009, 6:39 pm (T−00:09:00 hold) | 40%[31] | Phase-1 Lightning warning at the launch site[NASA 11] |
| 6 | 15 Jul 2009, 6:03:10 pm | Success | 1 day 23 hours 12 minutes | 60%[32] |
On July 15, 2009, at 18:03:10 EDT, the launch was finally successful.[33] Upon reviewing the launch video footage, imagery analysts noted eight or nine instances of foam shedding from the External Tank.[34] The pictures of the external tank taken when jettisoning showed loss of foam in the intertank ribbing.[35] The chairman of the Mission Management Team was not concerned and felt that the Space Shuttle would be cleared for re-entry on its return voyage—which it was a few days later.[36][37][NASA 12]The payload doors were opened after reaching orbit followed by deployment of theKu band antenna and activation of theshuttle's mechanical arm.[38]
The thermal protection system was inspected with the Shuttle Robotic Arm/Orbiter Boom Sensor System (OBSS) and the voluminous data downlinked for analysis. The orbital maneuvering system pods were inspected for tile damage or protruding tiles. The extravehicular mobility units were checked in addition to the rendezvous system tests and centerline camera installation. In preparation for the docking, the docking ring was extended.[38][NASA 13]
The shuttle successfully docked with the station 220 miles (350 km) above the Earth, following rendezvous pitch maneuver (RPM) photography ofEndeavour's thermal protection system by the Expedition 20 Crew.[39] During this procedure, the shuttle flips over on its back to the station so that the station crew can capture high resolution imagery of the underside of the shuttle. The docking happened on the ISS's PMA-2 (Pressurized Mating Adapter) on theHarmony module and the hatch was opened after leak checks. As part of the crew swap, station crew member Koichi Wakata was replaced with Tim Kopra. The two astronauts specially fitted seatliners were interchanged.[NASA 14] As part of preparation for EVA 1, astronauts Wolf and Kopra camped out in the Quest airlock. A quick review of the RPM imagery showed no serious concerns beyond two instances of coating loss. Further analysis of the imagery will be done. A boost of the station was completed with the shuttle's vernier thrusters to avoid a piece of space debris. The SRBs were retrieved and their camera imagery is expected to give more detail on the ET foam shedding.[15]
EVA 1 started with astronauts Dave Wolf and Tim Kopra switching their spacesuit power to internal battery at 16:19 UTC. Despite a communication problem with the spacewalkers, the Japanese Exposed Facility was successfully installed on the Japanese Experiment Module by means of a complex series of steps involving the robotic arms of both the station and the shuttle.[NASA 15] The JEF was first unberthed from the shuttle payload bay by the station arm, after which the shuttle arm took the load. The station arm was then moved to the worksite on Node-2 (Harmony), wherefrom it took the 4.1 ton facility back. The facility was then successfully latched on to the Experiment Module.[40][41][42] As part of the EVA, the spacewalkers successfully deployed the port Unpressurized Cargo Carrier Attach System (UCCAS), which could not be deployed duringSTS-119. During the prior mission, the deployment failed due to a jamming caused by a stuck detent pin. Engineers designed a custom tool to force the pin to release, which was used to deploy the mechanism.[43] Meanwhile, the shuttle managers announced that there would be no need for a focused inspection of the heat shield. The nose cap and wing leading-edge panels of the shuttle were cleared for entry as they were, but a reentry clearance was not given.[NASA 15] Beyond one impact site having a gouge, the rest of the impacts were found to be mostly a loss of coating.[44] The other activity scheduled for EVA 1, the deployment of a starboard side cargo carrier, was postponed for want of time.[43] A fuel cell issue found before launch was analyzed, though the cell continued to function as expected with no impact to the mission.[40]
The installation of the Integrated Cargo Carrier-Vertical Light Deployable (ICC-VLD) on the port side of the station was successfully completed with the use of both the shuttle and station robotic arms. The cargo pallet, containing spares and fresh batteries for the station, was lifted out of the shuttle bay by the shuttle arm and handed off to the station's Canadarm2, which maneuvered it to its position. The pallet's contents will be set up in upcoming EVAs. A malfunction in a new toilet in the Destiny laboratory caused the crew to use the one in the Russian segment while attempts were made to identify the fault. Meanwhile, the shuttle was cleared for reentry.[NASA 16][45][46][47]
Astronauts Wolf and Marshburn began EVA 2 at 15:27 UTC out of the Quest airlock. The EVA was to transfer the spare components brought by the shuttle from the ICC-VLD toExternal Stowage Platform-3. The spares were handled by Wolf riding the station's robotic arm to the P3 truss stowage platform where he and Marshburn attached them for long-term storage. The purpose of the spares was to provide redundancy to the station in the period following the shuttle's retirement. The spares unloaded include a Ku-Band Space-to-Ground antenna, a pump module for the coolant system and a drive unit for the station's robotic arm's mobile transporter. A planned installation of a camera on the Japanese Experiment Facility was postponed to a future EVA for want of time. Meanwhile, the malfunctioning toilet was set right with the replacement of internal parts and cleared for normal use after tests.[NASA 17][48][49][50]
.jpg)
In one of the more relaxed days, the Japanese logistics carrier was attached to the Japanese Exposed Facility. The cargo pallet was unberthed from the shuttle by the shuttle's robotic arm and handed to the station's robotic arm which then soft fixed it temporarily to the facility. After the experiments, containing an X-ray astronomy payload, a space environment monitor and a communications system, are installed the pallet will be returned to Earth by the shuttle.[NASA 18][51]
The spacewalk involving astronauts Wolf and Cassidy started at 14:32 UTC. As part of preparation for experiment installation on the Japanese external science deck, Cassidy removed the thermal covers off the experiment carrier. Meanwhile, Wolf removed obstructions, consisting of a steel handrail and an equipment installation socket, from theHarmony node to clear the way for an upcoming Japanese automated resupply ship. The other task for EVA 3, involving replacement of four of the six batteries in the P6 truss, did not go as planned. Each 170 kg (375 lb) battery was to be removed and placed in a temporary stowage platform while a new one is taken from the ICC-VLD and fixed. The old ones will be returned to Earth. When two new batteries had been installed and three old ones removed, the CO2 levels in Cassidy's suit showed an upward trend. Even though it never exceeded the safety limits, the EVA was called off with both astronauts returning into the station. This left one old battery in a temporary flexible stowage position. The rest of the batteries will be installed in a future EVA with the rest of the EVAs being under replanning.[NASA 19][52][53][54]
TheKibō robotic arm was inaugurated operationally with it being used to install experiments on to the Japanese exposed facility. The three experiments, transferred from the Japanese cargo pallet, consisted ofMonitor of All-sky X-ray Image, Inter-orbit Communication System and Space Environment Data Acquisition Equipment-Attached Payload. As per the revised plan for EVA 4 astronauts Cassidy and Marshburn will replace the remaining four batteries on P6 and complete the already deferred installation of a camera on the Japanese experiment facility.[NASA 20][NASA 21][55]
The fourth spacewalk, by Cassidy and Marshburn, involved replacement of the final four of the six batteries on P6 truss integrated electronics assembly. After berthing the old batteries in the ICC-VLD, the cargo pallet was returned to theEndeavour's payload bay by the shuttle's robotic arm. The elevated levels of CO2 in Cassidy's suit during EVA 3 was attributed to the astronaut working at a fast pace.[NASA 22][56][57]
The crew of both the shuttle and station had a day off. The day was uneventful except for the station's American CO2 removal system shutting down without any immediate impact.[NASA 23][58][59]
The Japanese Exposed Section cargo carrier was berthed inEndeavour's payload bay by the shuttle's robotic arm after it was handed the pallet by the station's robotic arm. After this the crew of both the station and the shuttle held a joint news conference. Meanwhile, the malfunctioning American CO2 removal system has been transitioned to manual mode in order to keep it running.[NASA 24][60][61]
Cassidy and Marshburn started EVA 5 at 11:33 UTC when they switched their suit power to internal battery. For this spacewalk, the CO2 absorbent system in the suits were changed fromLithium Hydroxide to METOX due to problems with Cassidy's usage. Cassidy completed the reconfiguring of power channels in the Zenith 1 patch panel which are used for the control moment gyroscopes. Before the rewiring, two of the gyroscopes were fed by the same power channel. Since a failure of the channel can knock down two gyros and put the station in a degraded position the reconfiguration was made necessary. This rewiring made the two gyros to operate from separate power channels. Meanwhile, Marshburn secured some multi-layered insulation on the Dextre. Later both the spacewalkers installed video cameras on the front and back of the Japanese exposed facility which will be used in dockings of the Japanese cargo crafts and normal operation. The cameras flew up in launch configuration and now have been installed in an operational configuration, thus completing the JEF assembly. Meanwhile, due to Cassidy's METOX limitation, the deployment of the PAS was deferred to a future spacewalk. Instead some get ahead tasks were completed which included installation of handrails and a portable foot restraint.[NASA 25][62][63][64][65]
After a crew farewellEndeavour undocked from the ISS at 17:26 UTC. Unlike most other launches, hatch closure, which happened at 15:08 UTC, and undocking happened on the same day due to the extended delay in launching and the arrival of theProgress 34 cargo craft. After undocking Hurley began a fly around of the station giving the shuttle crew an opportunity to photograph the station's current configuration in all directions. Then a final separation burn was completed at 3:09 pm EDT.[NASA 26][66][67]
The OBSS was grappled by the shuttle's robotic arm and used to inspectEndeavour's thermal protection system for damage from orbital debris. The imagery will be analyzed to clear the shuttle for reentry.[NASA 27] Meanwhile, the foam loss on the external tank was initially attributed to substrate contamination ahead of the application of the foam.[68] Later during the processing ofSTS-128, voids in the foam was highlighted as a trigger for the shedding. The air trapped in the voids could have expanded due to the high temperatures generated during ascent thus breaking the foam.[69][70]
The crew checked out the shuttle's systems for the landing, and successfully deployed theDRAGONSat and ANDE-2 satellites. The shuttle was cleared for reentry, with the TPS imagery showing no concerns.[NASA 28][71][72] The shuttle tracked two chances of landing at KSC on July 31, and could land no later due to its limitedcarbon dioxide-scrubbing LiOH supply.[73]
After a 16-day mission,Endeavour landed successfully at Kennedy Space Center at 10:48 EDT on July 31, 2009. The landing had to be undertaken before August 1, due to CO2-scrubbinglithium hydroxide limitations. There were two opportunities to land on July 31, of which the first was ultimately utilized.[NASA 29][74]
Fivespacewalks were conducted during STS-127.[NASA 1]
| EVA | Spacewalkers | Start (UTC) | End (UTC) | Duration |
|---|---|---|---|---|
| EVA 1 | David A. Wolf Timothy Kopra | July 18, 2009 16:19 | July 18, 2009 20:51 | 5 hours, 32 minutes |
| JEF installed andP3 NadirUnpressurized Cargo Carrier Attach System deployed. TheS3 Zenith OutboardPayload Attachment System deployment was postponed due to time constraints.[NASA 1][NASA 15][40][43] | ||||
| EVA 2 | Wolf Thomas H. Marshburn | July 20, 2009 15:27 | July 20, 2009 22:20 | 6 hours, 53 minutes |
| TransferredOrbital Replacement Units (ORUs) from theShuttle Integrated Cargo Carrier (ICC) to theExternal Stowage Platform-3 (ESP3). Transferred materials included a spare high-gain antenna, cooling-system pump module and spare parts for theMobile Servicing System. TheJEF Visual Equipment (JEF-VE) installation on the forward section was postponed due to time constraints.[NASA 17][48][49] | ||||
| EVA 3 | Wolf Christopher J. Cassidy | July 22, 2009 14:32 | July 22, 2009 20:31 | 5 hours, 59 minutes |
| JPM preparation work, ICS-EF MLI, andP6 battery replacement (2 of 6 units).[NASA 1] EVA was cut short due to high levels of CO2 in Cassidy's suit.[NASA 19][52][53] | ||||
| EVA 4 | Cassidy Marshburn | July 24, 2009 13:54 | July 24, 2009 21:06 | 7 hours, 12 minutes |
| P6 battery replacement (final 4 of 6).[NASA 22][56][57] | ||||
| EVA 5 | Cassidy Marshburn | July 27, 2009 11:33 | July 27, 2009 16:27 | 4 hours, 54 minutes |
| SPDM thermal cover adjustment,Z1 patch panel reconfiguration,JEM visual equipment (JEM-VE) installation (forward and aft), and JEM-LTA reconfigurations. The S3 NadirPayload Attachment System (outboard) deployment was postponed to a later mission.[NASA 25][62][63][64][NASA 30] | ||||
NASA began a tradition of playing music to astronauts during theGemini program, and first used music to wake up a flight crew duringApollo 15. Each track is specially chosen, often by the astronauts' families, and usually has a special meaning to an individual member of the crew, or is applicable to their daily activities.[NASA 31][NASA 32]
This article incorporatespublic domain material from websites or documents of theNational Aeronautics and Space Administration.
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