LDEF (Postflight), NASA history collection

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LDEF (Postflight), NASA history collection

LDEF (Postflight), NASA history collection

CAPE CANAVERAL, Fla. – At the Astrotech payload processing facility near NASA's Kennedy Space Center in Florida, workers at left guide the shipping cage removed from around NASA's Lunar CRater Observation and Sensing Satellite, known as LCROSS, at right. The satellite's primary mission is to search for water ice on the moon in a permanently shadowed crater near one of the lunar poles. LCROSS is a low-cost, accelerated-development, companion mission to NASA's Lunar Reconnaissance Orbiter, or LRO. At Kennedy, the two spacecraft will be integrated with an Atlas V launch vehicle and tested for final flight worthiness. LCROSS and LRO are the first missions in NASA's plan to return humans to the moon and begin establishing a lunar outpost by 2020. Launch is no earlier than April 24. Photo credit: NASA/Tim Jacobs KSC-2009-1744

CAPE CANAVERAL, Fla. – At the Astrotech payload processing facility near NASA's Kennedy Space Center in Florida, workers at left guide the shipping cage removed from around NASA's Lunar CRater Observation and Sensing Satellite, known as LCROSS, at right. The satellite's primary mission is to search for water ice on the moon in a permanently shadowed crater near one of the lunar poles. LCROSS is a low-cost, accelerated-development, companion mission to NASA's Lunar Reconnaissance Orbiter, or LRO. At Kennedy, the two spacecraft will be integrated with an Atlas V launch vehicle and tested for final flight worthiness. LCROSS and LRO are the first missions in NASA's plan to return humans to the moon and begin establishing a lunar outpost by 2020. Launch is no earlier than April 24. Photo credit: NASA/Tim Jacobs KSC-2009-1744

CAPE CANAVERAL, Fla. – In the Payload Hazardous Servicing Facility at NASA's Kennedy Space Center, the Multi-Use Lightweight Equipment, or MULE, carrier rests on a stand in the high bay. The MULE is part of the payload for the fifth and final shuttle servicing mission to NASA's Hubble Space Telescope, STS-125. The MULE carrier will join the Flight Support System, the Super Lightweight Interchangeable Carrier and the Orbital Replacement Unit Carrier in the Payload Hazardous Servicing Facility where the Hubble payload is being prepared for launch. The Relative Navigation Sensors and the New Outer Blanket Layers will be on the MULE. 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/Jack Pfaller KSC-08pd2313

CAPE CANAVERAL, Fla. – In the Payload Hazardous Servicing Facility at NASA's Kennedy Space Center, the Multi-Use Lightweight Equipment, or MULE, carrier rests on a stand in the high bay. The MULE is part of the payload for the fifth and final shuttle servicing mission to NASA's Hubble Space Telescope, STS-125. The MULE carrier will join the Flight Support System, the Super Lightweight Interchangeable Carrier and the Orbital Replacement Unit Carrier in the Payload Hazardous Servicing Facility where the Hubble payload is being prepared for launch. The Relative Navigation Sensors and the New Outer Blanket Layers will be on the MULE. 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/Jack Pfaller KSC-08pd2313

NASA's Lunar Reconnaissance Orbiter (LRO) spacecraft

NASA's Lunar Reconnaissance Orbiter (LRO) spacecraft

KENNEDY SPACE CENTER, FLA. -- Inside the Spacecraft Assembly and Encapsulation Facility 2, a covered Microwave Anisotropy Probe (MAP) satellite is revealed after removal of the container (far right). MAP will undergo testing in the SAEF-2 before its scheduled launch June 30 from Cape Canaveral Air Force Station on a Delta II rocket into a lunar-assisted trajectory to the Sun-Earth for a 27-month mission (3 months transit, 24 months observing). The MAP instrument consists of a set of passively cooled microwave radiometers with 1.4x 1.6-meter diameter primary reflectors to provide the desired angular resolution. MAP measures small fluctuations in the temperature of the cosmic microwave background radiation to an accuracy of one millionth of a degree. These measurements should reveal the size, matter content, age, geometry and fate of the universe. They will also reveal the primordial structure that grew to form galaxies and will test ideas about the origins of these primordial structures. The MAP instrument will be continuously shaded from the Sun, Earth, and Moon by the spacecraft. It is a product of Goddard Space Flight Center in partnership with Princeton University KSC-01pp0887

KENNEDY SPACE CENTER, FLA. -- Inside the Spacecraft Assembly and Encapsulation Facility 2, a covered Microwave Anisotropy Probe (MAP) satellite is revealed after removal of the container (far right). MAP will undergo testing in the SAEF-2 before its scheduled launch June 30 from Cape Canaveral Air Force Station on a Delta II rocket into a lunar-assisted trajectory to the Sun-Earth for a 27-month mission (3 months transit, 24 months observing). The MAP instrument consists of a set of passively cooled microwave radiometers with 1.4x 1.6-meter diameter primary reflectors to provide the desired angular resolution. MAP measures small fluctuations in the temperature of the cosmic microwave background radiation to an accuracy of one millionth of a degree. These measurements should reveal the size, matter content, age, geometry and fate of the universe. They will also reveal the primordial structure that grew to form galaxies and will test ideas about the origins of these primordial structures. The MAP instrument will be continuously shaded from the Sun, Earth, and Moon by the spacecraft. It is a product of Goddard Space Flight Center in partnership with Princeton University KSC-01pp0887

CAPE CANAVERAL, Fla. – At Astrotech Space Operations in Titusville, Fla., workers maneuver the position of NASA's Solar Dynamics Observatory, or SDO, after its rotation. The SDO will be moved to a work stand. SDO is the first space weather research network mission in NASA's Living With a Star Program. The spacecraft's long-term measurements will give solar scientists in-depth information about changes in the sun's magnetic field and insight into how they affect Earth. In preparation for its anticipated November launch, engineers will perform a battery of comprehensive tests to ensure SDO can withstand the stresses and vibrations of the launch itself, as well as what it will encounter in the space environment after launch. Photo credit: NASA/Cory Huston KSC-2009-4025

CAPE CANAVERAL, Fla. – At Astrotech Space Operations in Titusville, Fla., workers maneuver the position of NASA's Solar Dynamics Observatory, or SDO, after its rotation. The SDO will be moved to a work stand. SDO is the first space weather research network mission in NASA's Living With a Star Program. The spacecraft's long-term measurements will give solar scientists in-depth information about changes in the sun's magnetic field and insight into how they affect Earth. In preparation for its anticipated November launch, engineers will perform a battery of comprehensive tests to ensure SDO can withstand the stresses and vibrations of the launch itself, as well as what it will encounter in the space environment after launch. Photo credit: NASA/Cory Huston KSC-2009-4025

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LDEF (Postflight), NASA history collection

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LDEF (Postflight) EL-1994-00288 LDEF (Postflight) The image provides an overall view of LDEF experiments located in Bays D , the bay adjacent to the center ring structure, thru Bay F in Rows 8, the upper row, thru Row 11, the lower row. The LDEF is mounted on the LDEF Assembly and Transport System (LATS) in the rotation mode. The surfaces shown were facing in the direction of the orbital velocity vector and therefore exposed to the higher flux levels of atomic oxygen. The view shows the surfaces immediately after the LDEF arrived in SAEF II and prior to initiation of deintegration operations. Most experiments other than the Debris experiment (S0001) appear to have been degraded by the erosion of thin film polymer samples and/or signifi- cant color changes. Erosion of the thin film polymer samples is extensive on experiments located in LDEF positions D09, D10, E08 and F09. The silver TEFLON_ thermal cover material on experiments located in the D11 and E10 positions appears opaque with randomly located dark circular spots that appear to be debris points of impact. The black painted surface on the experiment in the E09 location has eroded exposing the red primer while some of the white paints on experiment surfaces and the yellow paint on the scuff plate appear in near prelaunch condition.
NASA Identifier: NIX-EL-1994-00288

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1990
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