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Electronics Racks in upper level launch equipment room.
Workers at Launch Complex 17-A, Cape Canaveral Air Force Station, carefully maneuver the Delta rocket fairing as it closes in on the Mars Odyssey spacecraft. NASA’s latest explorer carries three scientific instruments to map the chemical and mineralogical makeup of Mars: a thermal-emission imaging system, a gamma ray spectrometer and a Martian radiation environment experiment. The imaging system will map the planet with high-resolution thermal images and give scientists an increased level of detail to help them understand how the mineralogy of the planet relates to the land forms. In addition, Odyssey will serve as a communications relay for U.S. and international landers arriving at Mars in 2003/2004. The Mars Odyssey is scheduled for launch aboard a Delta II rocket April 7, 2001, at 11:02 a.m. EST KSC01pp0704
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KENNEDY SPACE CENTER, FLA. -- At Launch Complex 17B, Cape Canaveral Air Station, the protective covering on the Mars Polar Lander is lifted up and out of the way. The lander, in the opening below, is being mated to the Boeing Delta II rocket that will launch it on Jan. 3, 1999. The lander is a solar-powered spacecraft designed to touch down on the Martian surface near the northern-most boundary of the south pole in order to study the water cycle there. The lander also will help scientists learn more about climate change and current resources on Mars, studying such things as frost, dust, water vapor and condensates in the Martian atmosphere. It is the second spacecraft to be launched in a pair of Mars Surveyor'98 missions. The first is the Mars Climate Orbiter, which was launched aboard a Delta II rocket from Launch Complex 17A on Dec. 11, 1998 KSC-98pc1889
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KENNEDY SPACE CENTER, FLA. - On Launch Pad 17-B at Cape Canaveral Air Force Station, the first half of the fairing, at left, is moved into place for installation around the MESSENGER (Mercury Surface, Space Environment, Geochemistry and Ranging) spacecraft. The fairing is a molded structure that fits flush with the outside surface of the upper stage booster and forms an aerodynamically smooth joint, protecting the spacecraft during launch. MESSENGER is scheduled to launch Aug. 2 aboard a Boeing Delta II rocket and is expected to enter Mercury orbit in March 2011. MESSENGER was built for NASA by the Johns Hopkins University Applied Physics Laboratory in Laurel, Md. KSC-04pd1569
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VANDENBERG AIR FORCE BASE, Calif. – NASA's Orbiting Carbon Observatory-2, or OCO-2, satellite sits atop a United Launch Alliance Delta II rocket prior to encapsulation in its payload fairing at Space Launch Complex 2 at Vandenberg Air Force Base in California. Launch is scheduled for 2:56 a.m. PDT 5:56 a.m. EDT on July 1. OCO-2 is NASA’s first mission dedicated to studying atmospheric carbon dioxide, the leading human-produced greenhouse gas driving changes in Earth’s climate. OCO-2 will provide a new tool for understanding the human and natural sources of carbon dioxide emissions and the natural "sinks" that absorb carbon dioxide and help control its buildup. The observatory will measure the global geographic distribution of these sources and sinks and study their changes over time. To learn more about OCO-2, visit http://oco.jpl.nasa.gov Photo credit: NASA/Mark Mackley KSC-2014-3014
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Summary
The original finding aid described this as:
Description: View of the area behind panel NOD3D1-02, including the Temperature and Humidity Control (THC) duct, the Moderate Temperature Loop (MTL) Three Way Mixing Valve (TWMV) and Low Temperature Loop (LTL) Nitrogen (N2) Interface Assembly (NIA). Photo was taken during Expedition 22 / STS-130 joint operations.
Subject Terms: STS-130, Expedition 22, Node 3, Ducts, Valves
Date Taken: 2/16/2010
Categories: Station Configuration
Interior_Exterior: Interior
Ground_Orbit: On-orbit
Element: Node 3
Original: Digital Still
Preservation File Format: TIFF
STS-130
Nothing Found.
Tags
node
deck
alcove
internal
view
sts 130 endeavour
nasa
high resolution
ultra high resolution
sts 130
moderate temperature loop
low temperature loop
tiff sts 130
deck alcove internal view
duct
valve
expedition
temperature
preservation file format
panel nod 3 d 1 02
humidity control
three way
station configuration
space program
Date
2010
Source
The U.S. National Archives
Link
Copyright info
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