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Bob Williams, an actor of Living Voices from Seattle, interfaces with slides and a recorded narration during a ceremony in honor of Martin Luther King Jr. Day at Naval Undersea Museum.

Bob Williams, an actor of Living Voices from Seattle, interfaces with ...

KEYPORT, Wash. (Jan. 11, 2016) Bob Williams, an actor of Living Voices from Seattle, interfaces with slides and a recorded narration during a ceremony in honor of Martin Luther King Jr. Day at Naval Undersea Mu... More

CAPE CANAVERAL, Fla. – In the Payload Hazardous Servicing Facility at NASA's Kennedy Space Center, a technician removes the protective cover from the Soft Capture and Rendezvous System, or SCRS. The SCRS will enable the future rendezvous, capture and safe disposal of Hubble by either a crewed or robotic mission. The SCRS greatly increases the current shuttle capture interfaces on Hubble, therefore significantly reducing the rendezvous and capture design complexities associated with the disposal mission. The SCRS comprises the Soft Capture Mechanism system and the Relative Navigation System and is part of the payload on the fifth and final Hubble servicing mission, STS-125, targeted for launch Oct. 8. Photo credit: NASA/Jack Pfaller KSC-08pd2385

CAPE CANAVERAL, Fla. – In the Payload Hazardous Servicing Facility at ...

CAPE CANAVERAL, Fla. – In the Payload Hazardous Servicing Facility at NASA's Kennedy Space Center, a technician removes the protective cover from the Soft Capture and Rendezvous System, or SCRS. The SCRS will ... More

CAPE CANAVERAL, Fla. – In the Payload Hazardous Servicing Facility at NASA's Kennedy Space Center, technicians check the sensors on the Soft Capture Mechanism (SCM), part of the Soft Capture and Rendezvous System, or SCRS, after mating of the SCM to the Flight Support System, or FSS, carrier. The SCRS will enable the future rendezvous, capture and safe disposal of NASA's Hubble Space Telescope by either a crewed or robotic mission. The ring-like device attaches to Hubble’s aft bulkhead. The SCRS greatly increases the current shuttle capture interfaces on Hubble, therefore significantly reducing the rendezvous and capture design complexities associated with the disposal mission. The FSS will join the Multi-Use Lightweight Equipment, or MULE, carrier, the Super Lightweight Interchangeable Carrier and the Orbital Replacement Unit Carrier as payload on space shuttle Atlantis's STS-125 mission. The payload is scheduled to go to Launch Pad 39A in mid-September to be installed into Atlantis' payload bay. Atlantis is targeted to launch Oct. 8 at 1:34 a.m. EDT. Photo credit: NASA/Troy Cryder KSC-08pd2445

CAPE CANAVERAL, Fla. – In the Payload Hazardous Servicing Facility at ...

CAPE CANAVERAL, Fla. – In the Payload Hazardous Servicing Facility at NASA's Kennedy Space Center, technicians check the sensors on the Soft Capture Mechanism (SCM), part of the Soft Capture and Rendezvous Syst... More

CAPE CANAVERAL, Fla. – In the Payload Hazardous Servicing Facility at NASA's Kennedy Space Center, the Soft Capture Mechanism (SCM), part of the Soft Capture and Rendezvous System, or SCRS, is being prepared for transfer to the Flight Support System, or FSS, carrier. The SCRS will enable the future rendezvous, capture and safe disposal of NASA's Hubble Space Telescope by either a crewed or robotic mission. The ring-like device attaches to Hubble’s aft bulkhead. The SCRS greatly increases the current shuttle capture interfaces on Hubble, therefore significantly reducing the rendezvous and capture design complexities associated with the disposal mission. The FSS will join the Multi-Use Lightweight Equipment, or MULE, carrier, the Super Lightweight Interchangeable Carrier and the Orbital Replacement Unit Carrier as payload on space shuttle Atlantis's STS-125 mission. The payload is scheduled to go to Launch Pad 39A in mid-September to be installed into Atlantis' payload bay. Atlantis is targeted to launch Oct. 8 at 1:34 a.m. EDT. Photo credit: NASA/Troy Cryder KSC-08pd2432

CAPE CANAVERAL, Fla. – In the Payload Hazardous Servicing Facility at...

CAPE CANAVERAL, Fla. – In the Payload Hazardous Servicing Facility at NASA's Kennedy Space Center, the Soft Capture Mechanism (SCM), part of the Soft Capture and Rendezvous System, or SCRS, is being prepared ... More

Nighttime scene of Gemini spacecraft being hoisted to top of Pad 19

Nighttime scene of Gemini spacecraft being hoisted to top of Pad 19

S65-23710 (14 April 1965) --- Nighttime scene showing the Gemini-4 spacecraft being hoisted to the white room at the top of the gantry at Pad 19 for soft mating with the Titan launch vehicle.

STS110-301-020 - STS-110 - View of the starboard side of the S0 Truss (Face 6) taken during STS-110

STS110-301-020 - STS-110 - View of the starboard side of the S0 Truss ...

The original finding aid described this as: Description: View of the starboard side of the S0 Truss (Face 6 - S003E6) taken during the STS-110 mission. Visible are Extravehicular Activity (EVA) handrail 3438,... More

STS110-301-011 - STS-110 - View of the starboard side of the S0 Truss (Face 1) taken during STS-110

STS110-301-011 - STS-110 - View of the starboard side of the S0 Truss ...

The original finding aid described this as: Description: View of the starboard side of the S0 Truss (Face 1 - S003E1) showing Worksite Interface (WIF) S0-04 taken during the STS-110 mission. Part of the Mobil... More

STS110-301-004 - STS-110 - View of the starboard side of the S0 Truss (Face 2) taken during STS-110

STS110-301-004 - STS-110 - View of the starboard side of the S0 Truss ...

The original finding aid described this as: Description: View of the starboard side of the S0 Truss (Face 2 - S003E2) showing Worksite Interface (WIF) S0-04 and Extravehicular Activity (EVA) handrails 3422, 34... More

STS110-301-002 - STS-110 - View of the starboard side of the S0 Truss (Face 1) taken during STS-110

STS110-301-002 - STS-110 - View of the starboard side of the S0 Truss ...

The original finding aid described this as: Description: View of the starboard side of the S0 Truss (Face 1 - S003E1) showing Worksite Interface (WIF) S0-03 taken during the STS-110 mission. The Mobile Transp... More

STS100-391-023 - STS-100 - Panel PMA2/02-05 with EVA handrail 413 and WIF 03 taken during STS-100

STS100-391-023 - STS-100 - Panel PMA2/02-05 with EVA handrail 413 and ...

The original finding aid described this as: Description: View of Pressurized Mating Adapter 2 (PMA2) showing Panel PMA2/02-05 with Space Vision System (SVS) targets, Extravehicular Activity (EVA) handrail 413,... More

STS110-301-012 - STS-110 - View of the starboard side of the S0 Truss (Face 1) taken during STS-110

STS110-301-012 - STS-110 - View of the starboard side of the S0 Truss ...

The original finding aid described this as: Description: View of the starboard side of the S0 Truss (Face 1 - S003E1) showing Worksite Interface (WIF) S0-04 taken during the STS-110 mission. Part of the Mobil... More

STS100-393-037 - STS-100 - View of the Worksite Interface (WIF) A1 of the Spacelab Pallet taken during STS-100

STS100-393-037 - STS-100 - View of the Worksite Interface (WIF) A1 of ...

The original finding aid described this as: Description: View of the Worksite Interface (WIF) A1 of the Spacelab Pallet (SLP) taken during the STS-100 mission. Subject Terms: Handling Equipment, Interfaces, P... More

STS110-301-003 - STS-110 - View of the starboard side of the S0 Truss (Faces 1 and 2) taken during STS-110

STS110-301-003 - STS-110 - View of the starboard side of the S0 Truss ...

The original finding aid described this as: Description: View of the starboard side of the S0 Truss (Faces 1 and 2 - S003E1 and S003E2) showing Worksite Interface (WIF) S0-04 and a target taken during the STS-... More

STS110-301-019 - STS-110 - View of the starboard side of the S0 Truss (Face 6) taken during STS-110

STS110-301-019 - STS-110 - View of the starboard side of the S0 Truss ...

The original finding aid described this as: Description: View of the starboard side of the S0 Truss (Face 6 - S003E6) taken during the STS-110 mission. Visible are Extravehicular Activity (EVA) handrails 3438... More

KENNEDY SPACE CENTER, FLA. - Workers in the Payload Changeout Room (PCR) at Launch Pad 39A are preparing to close the payload doors for flight on the Space Shuttle Atlantis, targeted for liftoff on Mission STS-79 around Sept. 12. The payloads in Atlantis' cargo bay will play key roles during the upcoming spaceflight, which will be highlighted by the fourth docking between the U.S. Shuttle and Russian Space Station Mir. Located in the aft (lowermost) area of the payload bay is the SPACEHAB Double Module, filled with supplies and other items slated for transfer to the Russian Space Station Mir as well as research equipment. The SPACEHAB is connected by tunnel to the Orbiter Docking System (ODS). This view looks directly at the top of the ODS and shows clearly the Androgynous Peripheral Docking System (APDS) that interfaces with the Docking Module on Mir to achieve a linkup.

KENNEDY SPACE CENTER, FLA. - Workers in the Payload Changeout Room (...

KENNEDY SPACE CENTER, FLA. - Workers in the Payload Changeout Room (PCR) at Launch Pad 39A are preparing to close the payload doors for flight on the Space Shuttle Atlantis, targeted for liftoff on Mission ST... More

KENNEDY SPACE CENTER, FLA. -- The orbiter Columbia completes the short journey from Orbiter Processing Facility Bay 1 to the Vehicle Assembly Building (VAB). During its approximately one-week stay inside the VAB, the spaceplane will be mated to the external tank and twin solid rocket boosters, and electrical and mechanical interfaces will be verified. Rollout to Launch Pad 39B is planned for Oct. 16, where the two primary payloads of the upcoming STS-80 mission -- the Wake Shield Facility-3 (WSF-3) and Orbiting and Retrievable Far and Extreme Ultraviolet Spectrograph-Shuttle Pallet Satellite-2 (ORFEUS-SPAS-2) -- will be installed. Liftoff on the final Shuttle flight of 1996 is targeted for no earlier than Nov 8 at 2:47 p.m. EST. KSC-96pc1160

KENNEDY SPACE CENTER, FLA. -- The orbiter Columbia completes the short...

KENNEDY SPACE CENTER, FLA. -- The orbiter Columbia completes the short journey from Orbiter Processing Facility Bay 1 to the Vehicle Assembly Building (VAB). During its approximately one-week stay inside the VA... More

KENNEDY SPACE CENTER, FLA. -- The orbiter Columbia completes the short journey from Orbiter Processing Facility Bay 1 to the Vehicle Assembly Building (VAB). During its approximately one-week stay inside the VAB, the spaceplane will be mated to the external tank and twin solid rocket boosters, and electrical and mechanical interfaces will be verified. Rollout to Launch Pad 39B is planned for Oct. 16, where the two primary payloads of the upcoming STS-80 mission -- the Wake Shield Facility-3 (WSF-3) and Orbiting and Retrievable Far and Extreme Ultraviolet Spectrograph-Shuttle Pallet Satellite-2 (ORFEUS-SPAS-2) -- will be installed. Liftoff on the final Shuttle flight of 1996 is targeted for no earlier than Nov 8 at 2:47 p.m. EST KSC-96pc1159

KENNEDY SPACE CENTER, FLA. -- The orbiter Columbia completes the short...

KENNEDY SPACE CENTER, FLA. -- The orbiter Columbia completes the short journey from Orbiter Processing Facility Bay 1 to the Vehicle Assembly Building (VAB). During its approximately one-week stay inside the VA... More

KENNEDY SPACE CENTER, FLA. -- The orbiter Columbia completes the short journey from Orbiter Processing Facility Bay 1 to the Vehicle Assembly Building (VAB). During its approximately one-week stay inside the VAB, the spaceplane will be mated to the external tank and twin solid rocket boosters, and electrical and mechanical interfaces will be verified. Rollout to Launch Pad 39B is planned for Oct. 16, where the two primary payloads of the upcoming STS-80 mission -- the Wake Shield Facility-3 (WSF-3) and Orbiting and Retrievable Far and Extreme Ultraviolet Spectrograph-Shuttle Pallet Satellite-2 (ORFEUS-SPAS-2) -- will be installed. Liftoff on the final Shuttle flight of 1996 is targeted for no earlier than Nov 8 at 2:47 p.m. EST KSC-96pc1158

KENNEDY SPACE CENTER, FLA. -- The orbiter Columbia completes the short...

KENNEDY SPACE CENTER, FLA. -- The orbiter Columbia completes the short journey from Orbiter Processing Facility Bay 1 to the Vehicle Assembly Building (VAB). During its approximately one-week stay inside the VA... More

KENNEDY SPACE CENTER, FLA. - Workers in KSC's Vertical Processing Facility make final adjustments to the Flight Support System (FSS) for STS-82, the second Hubble Space Telescope servicing mission. The FSS is reusable flight hardware that provides the mechanical, structural and electrical interfaces between HST, the space support equipment and the orbiter for payload retrieval and on-orbit servicing. Liftoff aboard Discovery is targeted Feb. 11 with a crew of seven.

KENNEDY SPACE CENTER, FLA. - Workers in KSC's Vertical Processing Fac...

KENNEDY SPACE CENTER, FLA. - Workers in KSC's Vertical Processing Facility make final adjustments to the Flight Support System (FSS) for STS-82, the second Hubble Space Telescope servicing mission. The FSS is... More

In the Vertical Processing Facility, the Chandra X-ray Observatory is lowered toward the Inertial Upper Stage (IUS) in a workstand beneath it. There it will be mated with the IUS and then undergo testing to validate the IUS/Chandra connections and to check the orbiter avionics interfaces. Following that, an end-to-end test (ETE) will be conducted to verify the communications path to Chandra, commanding it as if it were in space. With the world's most powerful X-ray telescope, Chandra will allow scientists from around the world to see previously invisible black holes and high-temperature gas clouds, giving the observatory the potential to rewrite the books on the structure and evolution of our universe. Chandra is scheduled for launch July 22 aboard Space Shuttle Columbia, on mission STS-93 KSC-99pp0622

In the Vertical Processing Facility, the Chandra X-ray Observatory is ...

In the Vertical Processing Facility, the Chandra X-ray Observatory is lowered toward the Inertial Upper Stage (IUS) in a workstand beneath it. There it will be mated with the IUS and then undergo testing to val... More

The Inertial Upper Stage (IUS) booster is lowered toward a workstand in Kennedy Space Center's Vertical Processing Facility. The IUS will be mated with the Chandra X-ray Observatory and then undergo testing to validate the IUS/Chandra connections and check the orbiter avionics interfaces. Following that, an end-to-end test (ETE) will be conducted to verify the communications path to Chandra, commanding it as if it were in space. With the world's most powerful X-ray telescope, Chandra will allow scientists from around the world to see previously invisible black holes and high-temperature gas clouds, giving the observatory the potential to rewrite the books on the structure and evolution of our universe. Chandra is scheduled for launch July 22 aboard Space Shuttle Columbia, on mission STS-93 KSC-99pp0619

The Inertial Upper Stage (IUS) booster is lowered toward a workstand i...

The Inertial Upper Stage (IUS) booster is lowered toward a workstand in Kennedy Space Center's Vertical Processing Facility. The IUS will be mated with the Chandra X-ray Observatory and then undergo testing to ... More

In the Vertical Processing Facility, the Chandra X-ray Observatory is lifted from its workstand in order to move it to the Inertial Upper Stage (IUS) nearby. After being mated, the two components will then undergo testing to validate the IUS/Chandra connections and check the orbiter avionics interfaces. Following that, an end-to-end test (ETE) will be conducted to verify the communications path to Chandra, commanding it as if it were in space. With the world's most powerful X-ray telescope, Chandra will allow scientists from around the world to see previously invisible black holes and high-temperature gas clouds, giving the observatory the potential to rewrite the books on the structure and evolution of our universe. Chandra is scheduled for launch July 22 aboard Space Shuttle Columbia, on mission STS-93 KSC-99pp0620

In the Vertical Processing Facility, the Chandra X-ray Observatory is ...

In the Vertical Processing Facility, the Chandra X-ray Observatory is lifted from its workstand in order to move it to the Inertial Upper Stage (IUS) nearby. After being mated, the two components will then unde... More

The Inertial Upper Stage (IUS) booster is moved toward a workstand in Kennedy Space Center's Vertical Processing Facility. The IUS will be mated with the Chandra X-ray Observatory and then undergo testing to validate the IUS/Chandra connections and check the orbiter avionics interfaces. Following that, an end-to-end test (ETE) will be conducted to verify the communications path to Chandra, commanding it as if it were in space. With the world's most powerful X-ray telescope, Chandra will allow scientists from around the world to see previously invisible black holes and high-temperature gas clouds, giving the observatory the potential to rewrite the books on the structure and evolution of our universe. Chandra is scheduled for launch July 22 aboard Space Shuttle Columbia, on mission STS-93 KSC-99pp0618

The Inertial Upper Stage (IUS) booster is moved toward a workstand in ...

The Inertial Upper Stage (IUS) booster is moved toward a workstand in Kennedy Space Center's Vertical Processing Facility. The IUS will be mated with the Chandra X-ray Observatory and then undergo testing to va... More

In the Vertical Processing Facility, the Chandra X-ray Observatory is revealed with its protective cover removed. Chandra is ready for mating with the Inertial Upper Stage (IUS) beneath it, to be followed by testing to validate the IUS/Chandra connections and to check the orbiter avionics interfaces. Following that, an end-to-end test (ETE) will be conducted to verify the communications path to Chandra, commanding it as if it were in space. With the world's most powerful X-ray telescope, Chandra will allow scientists from around the world to see previously invisible black holes and high-temperature gas clouds, giving the observatory the potential to rewrite the books on the structure and evolution of our universe. Chandra is scheduled for launch July 22 aboard Space Shuttle Columbia, on mission STS-93 KSC-99pp0624

In the Vertical Processing Facility, the Chandra X-ray Observatory is ...

In the Vertical Processing Facility, the Chandra X-ray Observatory is revealed with its protective cover removed. Chandra is ready for mating with the Inertial Upper Stage (IUS) beneath it, to be followed by te... More

In the Vertical Processing Facility, the Chandra X-ray Observatory is lowered onto the Inertial Upper Stage (IUS) beneath it. After the two components are mated, they will undergo testing to validate the IUS/Chandra connections and to check the orbiter avionics interfaces. Following that, an end-to-end test (ETE) will be conducted to verify the communications path to Chandra, commanding it as if it were in space. With the world's most powerful X-ray telescope, Chandra will allow scientists from around the world to see previously invisible black holes and high-temperature gas clouds, giving the observatory the potential to rewrite the books on the structure and evolution of our universe. Chandra is scheduled for launch July 22 aboard Space Shuttle Columbia, on mission STS-93 KSC-99pp0623

In the Vertical Processing Facility, the Chandra X-ray Observatory is ...

In the Vertical Processing Facility, the Chandra X-ray Observatory is lowered onto the Inertial Upper Stage (IUS) beneath it. After the two components are mated, they will undergo testing to validate the IUS/Ch... More

In the Vertical Processing Facility, the Chandra X-ray Observatory is moved toward the Inertial Upper Stage (IUS) in a workstand at right. There it will be mated with the IUS and then undergo testing to validate the IUS/Chandra connections and check the orbiter avionics interfaces. Following that, an end-to-end test (ETE) will be conducted to verify the communications path to Chandra, commanding it as if it were in space. With the world's most powerful X-ray telescope, Chandra will allow scientists from around the world to see previously invisible black holes and high-temperature gas clouds, giving the observatory the potential to rewrite the books on the structure and evolution of our universe. Chandra is scheduled for launch July 22 aboard Space Shuttle Columbia, on mission STS-93 KSC-99pp0621

In the Vertical Processing Facility, the Chandra X-ray Observatory is ...

In the Vertical Processing Facility, the Chandra X-ray Observatory is moved toward the Inertial Upper Stage (IUS) in a workstand at right. There it will be mated with the IUS and then undergo testing to validat... More

The Inertial Upper Stage (IUS) booster (right) is lifted out of its container after arriving at Kennedy Space Center's Vertical Processing Facility. The IUS will be mated with the Chandra X-ray Observatory (at left) and then undergo testing to validate the IUS/Chandra connections and check the orbiter avionics interfaces. Following that, an end-to-end test (ETE) will be conducted to verify the communications path to Chandra, commanding it as if it were in space. With the world's most powerful X-ray telescope, Chandra will allow scientists from around the world to see previously invisible black holes and high-temperature gas clouds, giving the observatory the potential to rewrite the books on the structure and evolution of our universe. Chandra is scheduled for launch July 22 aboard Space Shuttle Columbia, on mission STS-93 KSC-99pp0617

The Inertial Upper Stage (IUS) booster (right) is lifted out of its co...

The Inertial Upper Stage (IUS) booster (right) is lifted out of its container after arriving at Kennedy Space Center's Vertical Processing Facility. The IUS will be mated with the Chandra X-ray Observatory (at ... More

STS-93 Mission Specialists Catherine Coleman (left) and Michel Tognini of France (right), representing the Centre National d'Etudes Spatiales (CNES), look over material on the mission payload behind them, the Chandra X-ray Observatory. Chandra is being mated with the Inertial Upper Stage (IUS) before testing to validate the IUS/Chandra connections and to check the orbiter avionics interfaces. Following that, an end-to-end test (ETE) will be conducted to verify the communications path to Chandra, commanding it as if it were in space. With the world's most powerful X-ray telescope, Chandra will allow scientists from around the world to see previously invisible black holes and high-temperature gas clouds, giving the observatory the potential to rewrite the books on the structure and evolution of our universe. Chandra is scheduled for launch July 22 aboard Space Shuttle Columbia, on mission STS-93 KSC-99pp0626

STS-93 Mission Specialists Catherine Coleman (left) and Michel Tognini...

STS-93 Mission Specialists Catherine Coleman (left) and Michel Tognini of France (right), representing the Centre National d'Etudes Spatiales (CNES), look over material on the mission payload behind them, the C... More

Workers in the Vertical Processing Facility observe the lower end of the Inertial Upper Stage (IUS) that will be mated with the Chandra X-ray Observatory (out of sight above it). After the two components are mated, they will undergo testing to validate the IUS/Chandra connections and to check the orbiter avionics interfaces. Following that, an end-to-end test (ETE) will be conducted to verify the communications path to Chandra, commanding it as if it were in space. With the world's most powerful X-ray telescope, Chandra will allow scientists from around the world to see previously invisible black holes and high-temperature gas clouds, giving the observatory the potential to rewrite the books on the structure and evolution of our universe. Chandra is scheduled for launch July 22 aboard Space Shuttle Columbia, on mission STS-93 KSC-99pp0625

Workers in the Vertical Processing Facility observe the lower end of t...

Workers in the Vertical Processing Facility observe the lower end of the Inertial Upper Stage (IUS) that will be mated with the Chandra X-ray Observatory (out of sight above it). After the two components are ma... More

STS-93 Mission Specialists Catherine Coleman (left) and Michel Tognini of France (right), who represents the Centre National d'Etudes Spatiales (CNES), look over the controls for the Chandra X-ray Observatory. Chandra is being mated with the Inertial Upper Stage (IUS) before testing to validate the IUS/Chandra connections and to check the orbiter avionics interfaces. Following that, an end-to-end test (ETE) will be conducted to verify the communications path to Chandra, commanding it as if it were in space. With the world's most powerful X-ray telescope, Chandra will allow scientists from around the world to see previously invisible black holes and high-temperature gas clouds, giving the observatory the potential to rewrite the books on the structure and evolution of our universe. Chandra is scheduled for launch July 22 aboard Space Shuttle Columbia, on mission STS-93 KSC-99pp0627

STS-93 Mission Specialists Catherine Coleman (left) and Michel Tognini...

STS-93 Mission Specialists Catherine Coleman (left) and Michel Tognini of France (right), who represents the Centre National d'Etudes Spatiales (CNES), look over the controls for the Chandra X-ray Observatory. ... More

STS106-321-018 - STS-106 - Ventilation ducts and CBM interfaces in Node 1 and PMA2 during STS-106

STS106-321-018 - STS-106 - Ventilation ducts and CBM interfaces in Nod...

The original finding aid described this as: Description: Views of ventilation ducts and Common Berthing Mechanism (CBM) interfaces in Pressurized Mating Adapter 2 (PMA2) and Node 1 / Unity taken during the STS... More

STS106-321-007 - STS-106 - Ventilation ducts and CBM interfaces in Node 1 and PMA2 during STS-106

STS106-321-007 - STS-106 - Ventilation ducts and CBM interfaces in Nod...

The original finding aid described this as: Description: Views of ventilation ducts and Common Berthing Mechanism (CBM) interfaces in Pressurized Mating Adapter 2 (PMA2) and Node 1 / Unity taken during the STS... More

STS106-321-015 - STS-106 - Ventilation ducts and CBM interfaces in Node 1 and PMA2 during STS-106

STS106-321-015 - STS-106 - Ventilation ducts and CBM interfaces in Nod...

The original finding aid described this as: Description: Views of ventilation ducts and Common Berthing Mechanism (CBM) interfaces in Pressurized Mating Adapter 2 (PMA2) and Node 1 / Unity taken during the STS... More

STS106-321-010 - STS-106 - Ventilation ducts and CBM interfaces in Node 1 and PMA2 during STS-106

STS106-321-010 - STS-106 - Ventilation ducts and CBM interfaces in Nod...

The original finding aid described this as: Description: Views of ventilation ducts and Common Berthing Mechanism (CBM) interfaces in Pressurized Mating Adapter 2 (PMA2) and Node 1 / Unity taken during the STS... More

STS097-373-004 - STS-097 - WIF 018 on the Z1 Trus & the P6 Truss taken during the first EVA of STS-97

STS097-373-004 - STS-097 - WIF 018 on the Z1 Trus & the P6 Truss taken...

The original finding aid described this as: Description: View of Worksite Interface (WIF) 018 on the Z1 Truss and a portion of the P6 Truss taken during the first Extravehicular Activity (EVA) of the STS-97 mi... More

STS106-321-016 - STS-106 - Ventilation ducts and CBM interfaces in Node 1 and PMA2 during STS-106

STS106-321-016 - STS-106 - Ventilation ducts and CBM interfaces in Nod...

The original finding aid described this as: Description: Views of ventilation ducts and Common Berthing Mechanism (CBM) interfaces in Pressurized Mating Adapter 2 (PMA2) and Node 1 / Unity taken during the STS... More

STS106-321-014 - STS-106 - Ventilation ducts and CBM interfaces in Node 1 and PMA2 during STS-106

STS106-321-014 - STS-106 - Ventilation ducts and CBM interfaces in Nod...

The original finding aid described this as: Description: Views of ventilation ducts and Common Berthing Mechanism (CBM) interfaces in Pressurized Mating Adapter 2 (PMA2) and Node 1 / Unity taken during the STS... More

STS106-321-012 - STS-106 - Ventilation ducts and CBM interfaces in Node 1 and PMA2 during STS-106

STS106-321-012 - STS-106 - Ventilation ducts and CBM interfaces in Nod...

The original finding aid described this as: Description: Views of ventilation ducts and Common Berthing Mechanism (CBM) interfaces in Pressurized Mating Adapter 2 (PMA2) and Node 1 / Unity taken during the STS... More

STS106-321-009 - STS-106 - Ventilation ducts and CBM interfaces in Node 1 and PMA2 during STS-106

STS106-321-009 - STS-106 - Ventilation ducts and CBM interfaces in Nod...

The original finding aid described this as: Description: Views of ventilation ducts and Common Berthing Mechanism (CBM) interfaces in Pressurized Mating Adapter 2 (PMA2) and Node 1 / Unity taken during the STS... More

STS106-321-011 - STS-106 - Ventilation ducts and CBM interfaces in Node 1 and PMA2 during STS-106

STS106-321-011 - STS-106 - Ventilation ducts and CBM interfaces in Nod...

The original finding aid described this as: Description: Views of ventilation ducts and Common Berthing Mechanism (CBM) interfaces in Pressurized Mating Adapter 2 (PMA2) and Node 1 / Unity taken during the STS... More

STS106-321-013 - STS-106 - Ventilation ducts and CBM interfaces in Node 1 and PMA2 during STS-106

STS106-321-013 - STS-106 - Ventilation ducts and CBM interfaces in Nod...

The original finding aid described this as: Description: Views of ventilation ducts and Common Berthing Mechanism (CBM) interfaces in Pressurized Mating Adapter 2 (PMA2) and Node 1 / Unity taken during the STS... More

STS106-321-017 - STS-106 - Ventilation ducts and CBM interfaces in Node 1 and PMA2 during STS-106

STS106-321-017 - STS-106 - Ventilation ducts and CBM interfaces in Nod...

The original finding aid described this as: Description: Views of ventilation ducts and Common Berthing Mechanism (CBM) interfaces in Pressurized Mating Adapter 2 (PMA2) and Node 1 / Unity taken during the STS... More

STS106-321-019 - STS-106 - Ventilation ducts and CBM interfaces in Node 1 and PMA2 during STS-106

STS106-321-019 - STS-106 - Ventilation ducts and CBM interfaces in Nod...

The original finding aid described this as: Description: Views of ventilation ducts and Common Berthing Mechanism (CBM) interfaces in Pressurized Mating Adapter 2 (PMA2) and Node 1 / Unity taken during the STS... More

STS106-321-008 - STS-106 - Ventilation ducts and CBM interfaces in Node 1 and PMA2 during STS-106

STS106-321-008 - STS-106 - Ventilation ducts and CBM interfaces in Nod...

The original finding aid described this as: Description: Views of ventilation ducts and Common Berthing Mechanism (CBM) interfaces in Pressurized Mating Adapter 2 (PMA2) and Node 1 / Unity taken during the STS... More

KENNEDY SPACE CENTER, Fla. -- Space Shuttle Endeavour leaves the Vehicle Assembly Building high bay 3 (open door) atop a Mobile Launcher Platform and begins rolling to Launch Pad 39A via a crawler-transporter. The combined height of the Shuttle, MLP and transporter is 235.2 ft. Once at the pad, routine launch pad validations will commence, verifying all vehicle and facility interfaces. Endeavour is expected to lift off on mission STS-100 on April 19, carrying the Multi-Purpose Logistics Module Raffaello and the Canadian robotic arm, SSRMS, to the International Space Station KSC01pp0564

KENNEDY SPACE CENTER, Fla. -- Space Shuttle Endeavour leaves the Vehic...

KENNEDY SPACE CENTER, Fla. -- Space Shuttle Endeavour leaves the Vehicle Assembly Building high bay 3 (open door) atop a Mobile Launcher Platform and begins rolling to Launch Pad 39A via a crawler-transporter. ... More

KENNEDY SPACE CENTER, Fla. -- Viewed from across the turn basin at Launch Complex 39 area, Space Shuttle Endeavour leaves the Vehicle Assembly Building high bay 3 (open door) atop a Mobile Launcher Platform and begins rolling to Launch Pad 39A via a crawler-transporter. The combined height of the Shuttle, MLP and transporter is 235.2 ft. (71.6 m). Once at the pad, routine launch pad validations will commence, verifying all vehicle and facility interfaces. Endeavour is expected to lift off on mission STS-100 on April 19, carrying the Multi-Purpose Logistics Module Raffaello and the Canadian robotic arm, SSRMS, to the International Space Station KSC01padig173

KENNEDY SPACE CENTER, Fla. -- Viewed from across the turn basin at Lau...

KENNEDY SPACE CENTER, Fla. -- Viewed from across the turn basin at Launch Complex 39 area, Space Shuttle Endeavour leaves the Vehicle Assembly Building high bay 3 (open door) atop a Mobile Launcher Platform and... More

Space Shuttle Endeavour leaves the Vehicle Assembly Building high bay 3 (open door) atop a Mobile Launcher Platform and begins rolling to Launch Pad 39A via a crawler-transporter. The combined height of the Shuttle, MLP and transporter is 235.2 ft. (71.6 m). Once at the pad, routine launch pad validations will commence, verifying all vehicle and facility interfaces. Endeavour is expected to lift off on mission STS-100 on April 19, carrying the Multi-Purpose Logistics Module Raffaello and the Canadian robotic arm, SSRMS, to the International Space Station KSC01padig171

Space Shuttle Endeavour leaves the Vehicle Assembly Building high bay ...

Space Shuttle Endeavour leaves the Vehicle Assembly Building high bay 3 (open door) atop a Mobile Launcher Platform and begins rolling to Launch Pad 39A via a crawler-transporter. The combined height of the Shu... More

KENNEDY SPACE CENTER, Fla. -- Space Shuttle Endeavour leaves the Vehicle Assembly Building high bay 3 (open door) atop a Mobile Launcher Platform and begins rolling to Launch Pad 39A via a crawler-transporter. The combined height of the Shuttle, MLP and transporter is 235.2 ft. (71.6 m). Once at the pad, routine launch pad validations will commence, verifying all vehicle and facility interfaces. Endeavour is expected to lift off on mission STS-100 on April 19, carrying the Multi-Purpose Logistics Module Raffaello and the Canadian robotic arm, SSRMS, to the International Space Station KSC01padig172

KENNEDY SPACE CENTER, Fla. -- Space Shuttle Endeavour leaves the Vehic...

KENNEDY SPACE CENTER, Fla. -- Space Shuttle Endeavour leaves the Vehicle Assembly Building high bay 3 (open door) atop a Mobile Launcher Platform and begins rolling to Launch Pad 39A via a crawler-transporter. ... More

KENNEDY SPACE CENTER, Fla. -- Viewed from across the turn basin at Launch Complex 39 area, Space Shuttle Endeavour leaves the Vehicle Assembly Building high bay 3 (open door) atop a Mobile Launcher Platform and begins rolling to Launch Pad 39A via a crawler-transporter. The combined height of the Shuttle, MLP and transporter is 235.2 ft. (71.6 m). Once at the pad, routine launch pad validations will commence, verifying all vehicle and facility interfaces. Endeavour is expected to lift off on mission STS-100 on April 19, carrying the Multi-Purpose Logistics Module Raffaello and the Canadian robotic arm, SSRMS, to the International Space Station KSC01pp0565

KENNEDY SPACE CENTER, Fla. -- Viewed from across the turn basin at Lau...

KENNEDY SPACE CENTER, Fla. -- Viewed from across the turn basin at Launch Complex 39 area, Space Shuttle Endeavour leaves the Vehicle Assembly Building high bay 3 (open door) atop a Mobile Launcher Platform and... More

SENIOR AIRMAN Brandon Smith, an Electronic Computer and Switching Systems Journeyman of the 603rd Air Communications Squadron, Aviano AB, Italy, swaps out a suspected faulty magnetic focus card in an Operator Control Unit that interfaces an Air Controller with all functions of the Tactical Air Operations Module. The Tactical Air Operations Module is a mobile command and control center that is deployed in conjuction with the AN/TPS-75 Radar System. Both are assets of the 603rd which are vital in controlling the airspace in and around a forward deployed location

SENIOR AIRMAN Brandon Smith, an Electronic Computer and Switching Syst...

The original finding aid described this photograph as: Base: Aviano Air Base State: Pordenone Country: Italy (ITA) Scene Major Command Shown: USAFE Scene Camera Operator: SSGT Jeremiah Erickson Release St... More

SENIOR AIRMAN Daxton Newberry, an Electronic Computer and Switching Systems Journeyman of the 603rd Air Communications Squadron, Aviano AB, Italy, swaps out a suspected faulty magnetic focus card in an Operator Control Unit that interfaces an Air Controller with all functions of the Tactical Air Operations Module. The Tactical Air Operations Module is a mobile command and control center that is deployed in conjuction with the AN/TPS-75 Radar System. Both are assets of the 603rd which are vital in controlling the airspace in and around a forward deployed location

SENIOR AIRMAN Daxton Newberry, an Electronic Computer and Switching Sy...

The original finding aid described this photograph as: Base: Aviano Air Base State: Pordenone Country: Italy (ITA) Scene Major Command Shown: USAFE Scene Camera Operator: SSGT Jeremiah Erickson Release St... More

STS110-324-010 - STS-110 - View of the starboard side of the S0 Truss (Face 6) taken during STS-110

STS110-324-010 - STS-110 - View of the starboard side of the S0 Truss ...

The original finding aid described this as: Description: View of the starboard side of the S0 Truss (Face 6 - S003E6) showing Extravehicular Activity (EVA) handrails 3438 and 3443, Worksite Interfaces (WIF) S0... More

STS110-327-023 - STS-110 - View of WIF 44 and a GPS antenna on the S0 Truss taken during STS-110

STS110-327-023 - STS-110 - View of WIF 44 and a GPS antenna on the S0 ...

The original finding aid described this as: Description: View of Worksite Interface (WIF) 44, External Video Switch Unit and a Global Positioning System (GPS) antenna on the S0 Truss taken during the STS-110 m... More

STS110-327-032 - STS-110 - View of WIF 44, RPCM and a Video Switch Unit on the S0 Truss taken during STS-110

STS110-327-032 - STS-110 - View of WIF 44, RPCM and a Video Switch Uni...

The original finding aid described this as: Description: View of Worksite Interface (WIF) 44, Remote Power Control Modules (RPCM), External Video Switch Unit and Extravehicular Activity (EVA) handrail 3523 on ... More

STS112-708-088 - STS-112 - EVA 4 - MS Wolf works with Interface Umbilical Assembly on MT

STS112-708-088 - STS-112 - EVA 4 - MS Wolf works with Interface Umbili...

The original finding aid described this as: Description: View of STS-112 Mission specialist David Wolf working to removed and replaced the Interface Umbilical Assembly on the station's Mobile Transporter durin... More

STS110-327-004 - STS-110 - View of a MTS Strut, WIF and EVA Handrail on the S0 Truss taken during STS-110

STS110-327-004 - STS-110 - View of a MTS Strut, WIF and EVA Handrail o...

The original finding aid described this as: Description: View of a Module-to-Truss Structure (MTS) Strut, Worksite Interface (WIF) 19 and Extravehicular Activity (EVA) handrail 3486 on the S0 Truss taken durin... More

STS110-327-022 - STS-110 - View of WIF 44 and a GPS antenna on the S0 Truss taken during STS-110

STS110-327-022 - STS-110 - View of WIF 44 and a GPS antenna on the S0 ...

The original finding aid described this as: Description: View of Worksite Interface (WIF) 44, External Video Switch Unit and a Global Positioning System (GPS) antenna on the S0 Truss taken during the STS-110 m... More

STS110-327-001 - STS-110 - View of energy absorbers, MDM and WIF on the S0 Truss taken during STS-110

STS110-327-001 - STS-110 - View of energy absorbers, MDM and WIF on th...

The original finding aid described this as: Description: View of energy absorbers, the Mobile Transporter (MT) rail, Multiplexer / Demultiplexer 10E 106 (MDM-10E) and Worksite Interface (WIF) 21 on the S0 Trus... More

STS110-324-013 - STS-110 - View of UMA's on the Mobile Transporter taken during STS-110

STS110-324-013 - STS-110 - View of UMA's on the Mobile Transporter tak...

The original finding aid described this as: Description: View of the Mobile Transporter (MT) showing Umbilical Mechanism Assemblies 1 and 2 (UMA) Active 0005 and the S0 Truss showing Extravehicular Activity (E... More

STS110-327-017 - STS-110 - View of a DDCU and a WIF on the S0 Truss taken during STS-110

STS110-327-017 - STS-110 - View of a DDCU and a WIF on the S0 Truss ta...

The original finding aid described this as: Description: View of a Direct Current (DC) to DC Converter Unit - External (DDCU-E) with Micro-Square Fixtures H-1 and H-2 in locked position and Worksite Interface ... More

STS112-708-089 - STS-112 - EVA 4 - MS Wolf works with Interface Umbilical Assembly on MT

STS112-708-089 - STS-112 - EVA 4 - MS Wolf works with Interface Umbili...

The original finding aid described this as: Description: View of STS-112 Mission specialist David Wolf working to removed and replaced the Interface Umbilical Assembly on the station's Mobile Transporter durin... More

STS110-327-008 - STS-110 - View of energy absorbers and WIF 24 on the S0 Truss taken during STS-110

STS110-327-008 - STS-110 - View of energy absorbers and WIF 24 on the ...

The original finding aid described this as: Description: View of energy absorbers and Worksite Interface (WIF) 24 on the S0 Truss taken during the STS-110 mission. Subject Terms: Absorbers (Equipment), Energy... More

STS110-327-002 - STS-110 - View of energy absorbers and WIF 21 on the S0 Truss taken during STS-110

STS110-327-002 - STS-110 - View of energy absorbers and WIF 21 on the ...

The original finding aid described this as: Description: View of energy absorbers, the Mobile Transporter (MT) rail and Worksite Interface (WIF) 21 on the S0 Truss taken during the STS-110 mission. Subject Te... More

STS110-324-011 - STS-110 - View of the starboard side of the S0 Truss (Face 6) taken during STS-110

STS110-324-011 - STS-110 - View of the starboard side of the S0 Truss ...

The original finding aid described this as: Description: View of the starboard side of the S0 Truss (Face 6 - S003E6) showing Extravehicular Activity (EVA) handrails 3438 and 3443, Worksite Interfaces (WIF) S0... More

STS112-708-090 - STS-112 - EVA 4 - MS Wolf works with Interface Umbilical Assembly on MT

STS112-708-090 - STS-112 - EVA 4 - MS Wolf works with Interface Umbili...

The original finding aid described this as: Description: View of STS-112 Mission specialist David Wolf working to removed and replaced the Interface Umbilical Assembly on the station's Mobile Transporter durin... More

STS110-327-034 - STS-110 - View of WIF 44, a DDCU-E and a Video Switch Unit on the S0 Truss taken during STS-110

STS110-327-034 - STS-110 - View of WIF 44, a DDCU-E and a Video Switch...

The original finding aid described this as: Description: View of Worksite Interface (WIF) 44, a Direct Current (DC) to DC Converter Unit - External (DDCU-E), External Video Switch Unit and Extravehicular Activ... More

STS110-327-033 - STS-110 - View of WIF 44, RPCM and a Video Switch Unit on the S0 Truss taken during STS-110

STS110-327-033 - STS-110 - View of WIF 44, RPCM and a Video Switch Uni...

The original finding aid described this as: Description: View of Worksite Interface (WIF) 44, Remote Power Control Modules (RPCM), External Video Switch Unit and Extravehicular Activity (EVA) handrail 3523 on ... More

STS112-370-028 - STS-112 - PMA2 WIF, handrail and cables

STS112-370-028 - STS-112 - PMA2 WIF, handrail and cables

The original finding aid described this as: Description: Close-up view of PMA 2 (PMA2/02-05) with Worksite Interface (WIF) 03, handrail 04130, assorted cables and an SVS target in the frame. Subject Terms: Ca... More

STS110-324-001 - STS-110 - View of the starboard side of the S0 Truss (Face 6) taken during STS-110

STS110-324-001 - STS-110 - View of the starboard side of the S0 Truss ...

The original finding aid described this as: Description: View of the starboard side of the S0 Truss (Face 6 - S003E6) showing Extravehicular Activity (EVA) handrails 3412 and 3413, Worksite Interface (WIF) S0-... More

STS112-708-091 - STS-112 - EVA 4 - MS Wolf works with Interface Umbilical Assembly on MT

STS112-708-091 - STS-112 - EVA 4 - MS Wolf works with Interface Umbili...

The original finding aid described this as: Description: View of STS-112 Mission specialist David Wolf working to removed and replaced the Interface Umbilical Assembly on the station's Mobile Transporter durin... More

STS110-327-036 - STS-110 - View of UMA's, a WIF and EVA handrails on the S0 Truss taken during STS-110

STS110-327-036 - STS-110 - View of UMA's, a WIF and EVA handrails on t...

The original finding aid described this as: Description: View of the Mobile Transporter (MT) rail, Umbilical Mechanism Assemblies 1 and 2 (UMA), Extravehicular Activity (EVA) Handrails 3544 and Worksite Interf... More

STS110-324-003 - STS-110 - View of the starboard side of the S0 Truss (Face 1) taken during STS-110

STS110-324-003 - STS-110 - View of the starboard side of the S0 Truss ...

The original finding aid described this as: Description: View of the starboard side of the S0 Truss (Face 1 - S003E1) showing Extravehicular Activity (EVA) handrail, the Mobile Transporter (MT) rail and Worksi... More

STS110-327-030 - STS-110 - View of EVA handrails and an Avionics Panel on the S0 Truss taken during STS-110

STS110-327-030 - STS-110 - View of EVA handrails and an Avionics Panel...

The original finding aid described this as: Description: View of an Avionics Connector Panel, Target, Worksite Interface (WIF) 42, and Extravehicular Activity (EVA) handrails 3539, 3529 and 3530 on the S0 Tru... More

STS110-324-005 - STS-110 - View of the starboard side of the S0 Truss (Face 1) taken during STS-110

STS110-324-005 - STS-110 - View of the starboard side of the S0 Truss ...

The original finding aid described this as: Description: View of the starboard side of the S0 Truss (Face 1 - S003E1) showing Extravehicular Activity (EVA) handrail, the Mobile Transporter (MT) rail and Worksi... More

STS110-327-012 - STS-110 - View of a DDCU and a WIF on the S0 Truss taken during STS-110

STS110-327-012 - STS-110 - View of a DDCU and a WIF on the S0 Truss ta...

The original finding aid described this as: Description: View of a Direct Current (DC) to DC Converter Unit - External (DDCU-E) with Micro-Square Fixtures H-1 and H-2 in locked position and Worksite Interface ... More

STS110-327-029 - STS-110 - View of a Grapple Fixture and an Avionics Panel on the S0 Truss taken during STS-110

STS110-327-029 - STS-110 - View of a Grapple Fixture and an Avionics P...

The original finding aid described this as: Description: View of a Grapple Fixture, an Avionics Connector Panel, Target, Worksite Interface (WIF) 42, Module-to-Truss Structure (MTS) Strut and Extravehicular Ac... More

STS110-324-024 - STS-110 - View of an EVA Handrail and WIF on the S0 Truss taken during STS-110

STS110-324-024 - STS-110 - View of an EVA Handrail and WIF on the S0 T...

The original finding aid described this as: Description: View of Extravehicular Activity (EVA) handrail 3473 and Worksite Interface (WIF) 28 inside a bay on the S0 Truss taken during the STS-110 mission. Subj... More

STS110-327-013 - STS-110 - View of WIF 24 and the MT Rail on the S0 Truss taken during STS-110

STS110-327-013 - STS-110 - View of WIF 24 and the MT Rail on the S0 Tr...

The original finding aid described this as: Description: View of energy absorbers, Mobile Transporter (MT) rail and Worksite Interface (WIF) 24 on the S0 Truss taken during the STS-110 mission. Subject Terms:... More

STS110-324-006 - STS-110 - View of the starboard side of the S0 Truss (Face 1) taken during STS-110

STS110-324-006 - STS-110 - View of the starboard side of the S0 Truss ...

The original finding aid described this as: Description: View of the starboard side of the S0 Truss (Face 1 - S003E1) showing Extravehicular Activity (EVA) handrail 3432, a target and Worksite Interface (WIF) ... More

Mr. Jimmy Barnes, General Dynamics, and US Army (USA) Private (PVT) Warren B. Jones, Jr., 447th Signal Battalion, work together to assemble a mobile subscriber radio terminal that interfaces with the Army's tactical cell phone system

Mr. Jimmy Barnes, General Dynamics, and US Army (USA) Private (PVT) Wa...

The original finding aid described this photograph as: Base: Fort Gillem State: Georgia (GA) Country: United States Of America (USA) Scene Major Command Shown: TRADOC Scene Camera Operator: Claude Stalling... More

KENNEDY SPACE CENTER, FLA. - Astronaut Tim Kopra aids in Intravehicular Activity (IVA) constraints testing on the Italian-built Node 2, a future element of the International Space Station. The second of three Station connecting modules, the Node 2 attaches to the end of the U.S. Lab and provides attach locations for several other elements. Kopra is currently assigned technical duties in the Space Station Branch of the Astronaut Office, where his primary focus involves the testing of crew interfaces for two future ISS modules as well as the implementation of support computers and operational Local Area Network on ISS. Node 2 is scheduled to launch on mission STS-120, Station assembly flight 10A.

KENNEDY SPACE CENTER, FLA. - Astronaut Tim Kopra aids in Intravehicula...

KENNEDY SPACE CENTER, FLA. - Astronaut Tim Kopra aids in Intravehicular Activity (IVA) constraints testing on the Italian-built Node 2, a future element of the International Space Station. The second of three ... More

KENNEDY SPACE CENTER, FLA. - Astronaut Tim Kopra aids in Intravehicular Activity (IVA) constraints testing on the Italian-built Node 2, a future element of the International Space Station. The second of three Station connecting modules, the Node 2 attaches to the end of the U.S. Lab and provides attach locations for several other elements. Kopra is currently assigned technical duties in the Space Station Branch of the Astronaut Office, where his primary focus involves the testing of crew interfaces for two future ISS modules as well as the implementation of support computers and operational Local Area Network on ISS. Node 2 is scheduled to launch on mission STS-120, Station assembly flight 10A.

KENNEDY SPACE CENTER, FLA. - Astronaut Tim Kopra aids in Intravehicula...

KENNEDY SPACE CENTER, FLA. - Astronaut Tim Kopra aids in Intravehicular Activity (IVA) constraints testing on the Italian-built Node 2, a future element of the International Space Station. The second of three ... More

KENNEDY SPACE CENTER, FLA. - Astronaut Tim Kopra (second from right) talks with workers in the Space Station Processing Facility about the Intravehicular Activity (IVA) constraints testing on the Italian-built Node 2, a future element of the International Space Station. . The second of three Station connecting modules, the Node 2 attaches to the end of the U.S. Lab and provides attach locations for several other elements. Kopra is currently assigned technical duties in the Space Station Branch of the Astronaut Office, where his primary focus involves the testing of crew interfaces for two future ISS modules as well as the implementation of support computers and operational Local Area Network on ISS. Node 2 is scheduled to launch on mission STS-120, Station assembly flight 10A.

KENNEDY SPACE CENTER, FLA. - Astronaut Tim Kopra (second from right) t...

KENNEDY SPACE CENTER, FLA. - Astronaut Tim Kopra (second from right) talks with workers in the Space Station Processing Facility about the Intravehicular Activity (IVA) constraints testing on the Italian-built ... More

KENNEDY SPACE CENTER, FLA. - Astronaut Tim Kopra (facing camera) aids in Intravehicular Activity (IVA) constraints testing on the Italian-built Node 2, a future element of the International Space Station. The second of three Station connecting modules, the Node 2 attaches to the end of the U.S. Lab and provides attach locations for several other elements. Kopra is currently assigned technical duties in the Space Station Branch of the Astronaut Office, where his primary focus involves the testing of crew interfaces for two future ISS modules as well as the implementation of support computers and operational Local Area Network on ISS. Node 2 is scheduled to launch on mission STS-120, Station assembly flight 10A.

KENNEDY SPACE CENTER, FLA. - Astronaut Tim Kopra (facing camera) aids ...

KENNEDY SPACE CENTER, FLA. - Astronaut Tim Kopra (facing camera) aids in Intravehicular Activity (IVA) constraints testing on the Italian-built Node 2, a future element of the International Space Station. The ... More

KENNEDY SPACE CENTER, FLA. - Astronaut Tim Kopra talks to a technician (off-camera) during Intravehicular Activity (IVA) constraints testing on the Italian-built Node 2, a future element of the International Space Station. The second of three Station connecting modules, the Node 2 attaches to the end of the U.S. Lab and provides attach locations for several other elements. Kopra is currently assigned technical duties in the Space Station Branch of the Astronaut Office, where his primary focus involves the testing of crew interfaces for two future ISS modules as well as the implementation of support computers and operational Local Area Network on ISS. Node 2 is scheduled to launch on mission STS-120, Station assembly flight 10A.

KENNEDY SPACE CENTER, FLA. - Astronaut Tim Kopra talks to a technician...

KENNEDY SPACE CENTER, FLA. - Astronaut Tim Kopra talks to a technician (off-camera) during Intravehicular Activity (IVA) constraints testing on the Italian-built Node 2, a future element of the International Sp... More

KENNEDY SPACE CENTER, FLA. - In the Space Station Processing Facility, workers check over the Italian-built Node 2, a future element of the International Space Station. The second of three Station connecting modules, the Node 2 attaches to the end of the U.S. Lab and provides attach locations for several other elements. Kopra is currently assigned technical duties in the Space Station Branch of the Astronaut Office, where his primary focus involves the testing of crew interfaces for two future ISS modules as well as the implementation of support computers and operational Local Area Network on ISS. Node 2 is scheduled to launch on mission STS-120, Station assembly flight 10A.

KENNEDY SPACE CENTER, FLA. - In the Space Station Processing Facility,...

KENNEDY SPACE CENTER, FLA. - In the Space Station Processing Facility, workers check over the Italian-built Node 2, a future element of the International Space Station. The second of three Station connecting m... More

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, workers stand by as the left-hand Orbital Maneuvering System (OMS) pod is maneuvered toward the engine interfaces on the orbiter Discovery for installation. The Orbital Maneuvering System provides the thrust for orbit insertion, orbit circularization, orbit transfer, rendezvous, deorbit, abort to orbit and abort once around. It can provide up to 1,000 pounds of propellant to the aft reaction control system. Each pod contains one OMS engine and the hardware needed to pressurize, store and distribute the propellants to perform the velocity maneuvers. KSC-04pd0949

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, worke...

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, workers stand by as the left-hand Orbital Maneuvering System (OMS) pod is maneuvered toward the engine interfaces on the orbiter Discovery for in... More

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, the left-hand Orbital Maneuvering System (OMS) pod (top of photo) is poised behind the engine interfaces on the orbiter Discovery for installation. The Orbital Maneuvering System provides the thrust for orbit insertion, orbit circularization, orbit transfer, rendezvous, deorbit, abort to orbit and abort once around. It can provide up to 1,000 pounds of propellant to the aft reaction control system. Each pod contains one OMS engine and the hardware needed to pressurize, store and distribute the propellants to perform the velocity maneuvers. KSC-04pd0947

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, the ...

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, the left-hand Orbital Maneuvering System (OMS) pod (top of photo) is poised behind the engine interfaces on the orbiter Discovery for installati... More

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, the left-hand Orbital Maneuvering System (OMS) pod is maneuvered toward the engine interfaces on the orbiter Discovery for installation. The Orbital Maneuvering System provides the thrust for orbit insertion, orbit circularization, orbit transfer, rendezvous, deorbit, abort to orbit and abort once around. It can provide up to 1,000 pounds of propellant to the aft reaction control system. Each pod contains one OMS engine and the hardware needed to pressurize, store and distribute the propellants to perform the velocity maneuvers. KSC-04pd0948

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, the ...

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, the left-hand Orbital Maneuvering System (OMS) pod is maneuvered toward the engine interfaces on the orbiter Discovery for installation. The O... More

S120E007787 - STS-120 - S1 truss

S120E007787 - STS-120 - S1 truss

The original finding aid described this as: Description: View of thermal blankets and worksite interface (WIF) 15 in Bay 11 on the forward side of the S1 Truss as documented by the STS-120 crew. Subject Terms... More

S120E007784 - STS-120 - S3 truss

S120E007784 - STS-120 - S3 truss

The original finding aid described this as: Description: View of cables, connectors, handrail 3072 and worksite interface (WIF) 21 on the forward side of the S3 Truss as documented by the STS-120 crew. Subj... More

S120E007702 - STS-120 - Close-up view of PMA2

S120E007702 - STS-120 - Close-up view of PMA2

The original finding aid described this as: Description: Close-up view of cables, Worksite Interface (WIF) 03 and 02 on Nadir (+ZA) side of Pressurized Mating Adapter 2 (PMA2) at location code PMA2/02-05 as se... More

S118E07208 - STS-118 - Close-up view of the S0 Truss taken during STS-118

S118E07208 - STS-118 - Close-up view of the S0 Truss taken during STS-...

The original finding aid described this as: Description: Close-up view of Worksite Interface (WIF) 21 on the S0 truss. S0-2 MDM is visible Photo taken during the STS-118 mission. Subject Terms: STS-118, Tru... More

S120E007701 - STS-120 - Close-up view of PMA2

S120E007701 - STS-120 - Close-up view of PMA2

The original finding aid described this as: Description: Close-up view of cables, Worksite Interface (WIF) 03 and 02 on Nadir (+ZA) side of Pressurized Mating Adapter 2 (PMA2) at location code PMA2/02-05 as s... More

S120E007943 - STS-120 - P1 truss

S120E007943 - STS-120 - P1 truss

The original finding aid described this as: Description: View of Multilayer Insulation (MLI), worksite interfaces (WIF) and hand rails in Bay 8 of the P1 Truss as documented by the STS-120 crew. Subject Term... More

S124E008097 - STS-124 - S0 Truss

S124E008097 - STS-124 - S0 Truss

The original finding aid described this as: Description: Close-up view of Worsite Interface (WIF) 22 in Bay 00 of the S0 truss as documented by the STS-124 crew. Subject Terms: Trusses, STS-124, S0, Interface... More

S123E006246 - STS-123 - ISL Interface Panel on Node 2 taking during STS-123 / Expedition 16 Joint Operations

S123E006246 - STS-123 - ISL Interface Panel on Node 2 taking during ST...

The original finding aid described this as: Description: View of Integrated Station LAN (ISL) Interface Panel on Node 2. Photo was taken during STS-123 / Expedition 16 joint operations. Subject Terms: STS-12... More

S124E008089 - STS-124 - S0 Truss

S124E008089 - STS-124 - S0 Truss

The original finding aid described this as: Description: Close-up view of the area of Worksite Interface (WIF) 04 in Bay 03 of the S0 truss as documented by the STS-124 crew. Subject Terms: Trusses, STS-124, ... More

S124E008060 - STS-124 - SO Truss

S124E008060 - STS-124 - SO Truss

The original finding aid described this as: Description: Close-up view of ExtraVehicular Charged Particle Spectrometer (EVCPDS) and Work Site Interfaces (WIF) sockets on the S0 truss as documented by the STS-1... More

S124E008100 - STS-124 - S0 Truss

S124E008100 - STS-124 - S0 Truss

The original finding aid described this as: Description: Close-up view of Worksite Interface (WIF) 22 in Bay 00 of the S0 truss as documented by the STS-124 crew. Subject Terms: Trusses, STS-124, S0, Interfa... More

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