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Space Shuttle Project, Marshall Space Flight Center

Onboard Space Shuttle Columbia's (STS-87) first ever Extravehicular Activity (EVA), astronaut Takao Doi works with a 156-pound crane carried onboard for the first time. The crane's inclusion and the work with i More

Space Shuttle Project, Marshall Space Flight Center

Onboard Space Shuttle Columbia's (STS-87) first ever Extravehicular Activity (EVA), astronaut Takao Doi works with a 156-pound crane carried onboard for the first time. The crane's inclusion and the work with i More

Large ORU/ Crane evaluations conducted during first EVA of STS-87 (DTO 671)

STS087-718-069 (19 November ? 5 December 1997) --- On the Space Shuttle Columbia's first ever spacewalk (EVA), astronaut Takao Doi works with a 156-pound crane carried onboard for the first time this trip of Co More

Large ORU/ Crane evaluations conducted during first EVA of STS-87 (DTO 671)

STS087-718-073 (19 November ? 5 December 1997) --- On the Space Shuttle Columbia's first ever spacewalk (EVA), astronaut Winston E. Scott works with a simulated battery and 156-pound crane carried onboard for t More

KENNEDY SPACE CENTER, FLA. - Technicians attach a crane to the Pump Flow Control Subsystem (PFCS) in the Space Station Processing Facility. The PFCS pumps and controls the liquid ammonia used to cool the various Orbital Replacement Units on the Integrated Equipment Assembly that make up the S6 Photo-Voltaic Power Module on the International Space Station (ISS). The fourth starboard truss segment, the S6 Truss measures 112 feet long by 39 feet wide. Its solar arrays are mounted on a “blanket” that can be folded like an accordion for delivery to the ISS. Once in orbit, astronauts will deploy the blankets to their full size. When completed, the Station's electrical power system (EPS) will use eight photovoltaic solar arrays to convert sunlight to electricity. Delivery of the S6 Truss, the last power module truss segment, is targeted for mission STS-119. KSC-04pd1477

KENNEDY SPACE CENTER, FLA. - Technicians attach a crane to the Pump Flow Control Subsystem (PFCS) in the Space Station Processing Facility. The PFCS pumps and controls the liquid ammonia used to cool the vario More

KENNEDY SPACE CENTER, FLA. - In the Space Station Processing Facility, astronaut Tracy Caldwell (second from left) assists technicians position the Pump Flow Control Subsystem (PFCS) over the upper deck of the S6 Truss. The PFCS pumps and controls the liquid ammonia used to cool the various Orbital Replacement Units on the Integrated Equipment Assembly that make up the S6 Photo-Voltaic Power Module on the International Space Station (ISS). The fourth starboard truss segment, the S6 Truss measures 112 feet long by 39 feet wide. Its solar arrays are mounted on a “blanket” that can be folded like an accordion for delivery to the ISS. Once in orbit, astronauts will deploy the blankets to their full size. When completed, the Station's electrical power system (EPS) will use eight photovoltaic solar arrays to convert sunlight to electricity. Delivery of the S6 Truss, the last power module truss segment, is targeted for mission STS-119. KSC-04pd1480

KENNEDY SPACE CENTER, FLA. - In the Space Station Processing Facility, astronaut Tracy Caldwell (second from left) assists technicians position the Pump Flow Control Subsystem (PFCS) over the upper deck of the More

KENNEDY SPACE CENTER, FLA. - In the Space Station Processing Facility, astronaut Tracy Caldwell (left) assists technicians install the Pump Flow Control Subsystem (PFCS) onto the upper deck of the S6 Truss. The PFCS pumps and controls the liquid ammonia used to cool the various Orbital Replacement Units on the Integrated Equipment Assembly that make up the S6 Photo-Voltaic Power Module on the International Space Station (ISS). The fourth starboard truss segment, the S6 Truss measures 112 feet long by 39 feet wide. Its solar arrays are mounted on a “blanket” that can be folded like an accordion for delivery to the ISS. Once in orbit, astronauts will deploy the blankets to their full size. When completed, the Station's electrical power system (EPS) will use eight photovoltaic solar arrays to convert sunlight to electricity. Delivery of the S6 Truss, the last power module truss segment, is targeted for mission STS-119. KSC-04pd1482

KENNEDY SPACE CENTER, FLA. - In the Space Station Processing Facility, astronaut Tracy Caldwell (left) assists technicians install the Pump Flow Control Subsystem (PFCS) onto the upper deck of the S6 Truss. Th More

KENNEDY SPACE CENTER, FLA. - In the Space Station Processing Facility, astronaut Tracy Caldwell (left) assists a technician check out the Pump Flow Control Subsystem (PFCS) before it is installed on the upper deck of the S6 Truss. The PFCS pumps and controls the liquid ammonia used to cool the various Orbital Replacement Units on the Integrated Equipment Assembly that make up the S6 Photo-Voltaic Power Module on the International Space Station (ISS). The fourth starboard truss segment, the S6 Truss measures 112 feet long by 39 feet wide. The solar arrays are mounted on a “blanket” that can be folded like an accordion for delivery to the ISS. Once in orbit, astronauts will deploy the blankets to their full size. When completed, the Station's electrical power system (EPS) will use eight photovoltaic solar arrays to convert sunlight to electricity. Delivery of the S6 Truss, the last power module truss segment, is targeted for mission STS-119. KSC-04pd1478

KENNEDY SPACE CENTER, FLA. - In the Space Station Processing Facility, astronaut Tracy Caldwell (left) assists a technician check out the Pump Flow Control Subsystem (PFCS) before it is installed on the upper d More

KENNEDY SPACE CENTER, FLA. - In the Space Station Processing Facility, astronaut Tracy Caldwell (second from left) assists technicians lower the Pump Flow Control Subsystem (PFCS) into position onto the upper deck of the S6 Truss. The PFCS pumps and controls the liquid ammonia used to cool the various Orbital Replacement Units on the Integrated Equipment Assembly that make up the S6 Photo-Voltaic Power Module on the International Space Station (ISS). The fourth starboard truss segment, the S6 Truss measures 112 feet long by 39 feet wide. Its solar arrays are mounted on a “blanket” that can be folded like an accordion for delivery to the ISS. Once in orbit, astronauts will deploy the blankets to their full size. When completed, the Station's electrical power system (EPS) will use eight photovoltaic solar arrays to convert sunlight to electricity. Delivery of the S6 Truss, the last power module truss segment, is targeted for mission STS-119. KSC-04pd1481

KENNEDY SPACE CENTER, FLA. - In the Space Station Processing Facility, astronaut Tracy Caldwell (second from left) assists technicians lower the Pump Flow Control Subsystem (PFCS) into position onto the upper d More

KENNEDY SPACE CENTER, FLA. - Unpacking of the Pump Flow Control Subsystem (PFCS) begins in the Space Station Processing Facility. The PFCS pumps and controls the liquid ammonia used to cool the various Orbital Replacement Units on the Integrated Equipment Assembly that make up the S6 Photo-Voltaic Power Module on the International Space Station (ISS). The fourth starboard truss segment, the S6 Truss measures 112 feet long by 39 feet wide. Its solar arrays are mounted on a “blanket” that can be folded like an accordion for delivery to the ISS. Once in orbit, astronauts will deploy the blankets to their full size. When completed, the Station's electrical power system will use eight photovoltaic solar arrays to convert sunlight to electricity. Delivery of the S6 Truss, the last power module truss segment, is targeted for mission STS-119. KSC-04pd1476

KENNEDY SPACE CENTER, FLA. - Unpacking of the Pump Flow Control Subsystem (PFCS) begins in the Space Station Processing Facility. The PFCS pumps and controls the liquid ammonia used to cool the various Orbital More

KENNEDY SPACE CENTER, FLA. - In the Space Station Processing Facility, a technician steadies the Pump Flow Control Subsystem (PFCS) as it is lifted and moved toward the S6 Truss. The PFCS pumps and controls the liquid ammonia used to cool the various Orbital Replacement Units on the Integrated Equipment Assembly that make up the S6 Photo-Voltaic Power Module on the International Space Station (ISS). The fourth starboard truss segment, the S6 Truss measures 112 feet long by 39 feet wide. Its solar arrays are mounted on a “blanket” that can be folded like an accordion for delivery to the ISS. Once in orbit, astronauts will deploy the blankets to their full size. When completed, the Station's electrical power system (EPS) will use eight photovoltaic solar arrays to convert sunlight to electricity. Delivery of the S6 Truss, the last power module truss segment, is targeted for mission STS-119. KSC-04pd1479

KENNEDY SPACE CENTER, FLA. - In the Space Station Processing Facility, a technician steadies the Pump Flow Control Subsystem (PFCS) as it is lifted and moved toward the S6 Truss. The PFCS pumps and controls th More

S126E008432 - STS-126 - WRS Configuration in US Lab

The original finding aid described this as: Description: View of a portion of the Water Recovery System 2 (WRS2) rack in the U.S. Laboratory / Destiny module, including the Fluids Control and Pump Assembly (FC More

S126E008585 - STS-126 - WRS Initialization in US Lab

The original finding aid described this as: Description: Documentation of a portion of the Water Recovery System 1 (WRS1), including the Particulate Filter (PF), Microbial Check Valve (MCV), Reactor Health Sen More

S126E008395 - STS-126 - WRS Configuration in US Lab

The original finding aid described this as: Description: View of a portion of Water Recovery System 1 (WRS1) rack in the U.S. Laboratory / Destiny module, including the Gas Separator (GS) and Catalytic Reactor More

S126E008451 - STS-126 - WRS Configuration in US Lab

The original finding aid described this as: Description: View of the Waste Water (WW) and Multifiltration Bed 1 (MFB1) Orbital Replacement Units (ORUs) in the Water Recovery System 2 (WRS2) rack in the U.S. La More

S126E008399 - STS-126 - WRS Configuration in US Lab

The original finding aid described this as: Description: View of a portion of Water Recovery System 1 (WRS1) rack in the U.S. Laboratory / Destiny module, including the Particulate Filter (PF) and Area Smoke D More

S126E008429 - STS-126 - WRS Configuration in US Lab

The original finding aid described this as: Description: View of a portion of the Water Recovery System 2 (WRS2) rack in the U.S. Laboratory / Destiny module, including the Recycle Filter Tank Assembly (RFTA), More

S126E008430 - STS-126 - WRS Configuration in US Lab

The original finding aid described this as: Description: View of a portion of the Water Recovery System 2 (WRS2) rack in the U.S. Laboratory / Destiny module, including the Recycle Filter Tank Assembly (RFTA), More

S126E008396 - STS-126 - WRS Configuration in US Lab

The original finding aid described this as: Description: View of a portion of Water Recovery System 1 (WRS1) rack in the U.S. Laboratory / Destiny module, including the Reactor Health Sensor (RHS) and Microbia More

S126E008428 - STS-126 - WRS Configuration in US Lab

The original finding aid described this as: Description: View of a portion of the Water Recovery System 2 (WRS2) rack in the U.S. Laboratory / Destiny module, including the Wastewater Storage Tank Assembly (WS More

S126E008402 - STS-126 - WRS Configuration in US Lab

The original finding aid described this as: Description: View of a portion of Water Recovery System 1 (WRS1) rack in the U.S. Laboratory / Destiny module, including the Avionics Air Assembly (AAA) and Ion Exch More

S126E008394 - STS-126 - WRS Configuration in US Lab

The original finding aid described this as: Description: View of a portion of Water Recovery System 1 (WRS1) rack in the U.S. Laboratory / Destiny module, including the Particulate Filter (PF), Reactor Health More

S126E008397 - STS-126 - WRS Configuration in US Lab

The original finding aid described this as: Description: View of a portion of Water Recovery System 1 (WRS1) rack in the U.S. Laboratory / Destiny module, including the Reactor Health Sensor (RHS) and Microbia More

S126E008409 - STS-126 - WRS Configuration in US Lab

The original finding aid described this as: Description: View of the Wastewater Storage Tank Assembly (WSTA) and Separator Plumbing Assembly (SPA) Orbital Replacement Units (ORUs) on the Water Recovery System More