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Cape Canaveral Air Force Station, Launch Complex 39, Mobile Launcher Platforms, Launcher Road, East of Kennedy Parkway North, Cape Canaveral, Brevard County, FL

Darracq 30 hp water-cooled flat-twin aircraft engine Flight 23 October 1909

A steam engine sitting inside of a building. Engine boat fisherman.

TEST RIG SET UP FOR ALLIED SIGNAL

STS092-354-018 - STS-092 - Node 1 Forward CBM latches/alignment guides

STS110-334-028 - STS-110 - View of the aft avionics tray between the Z1 and S0 Trusses taken during the fourth EVA of STS-110

The Royal Navy on the Home Front, 1914-1918 Q18868

CHAMBER NO. 075 ON STAND AT THE ROCKET ENGINE TEST FACILITY RETF

S130E007642 - STS-130 - Node 3 Vestibule Outfitting

code Related

S126E008431 - STS-126 - WRS Configuration in US Lab

S126E008421 - STS-126 - WRS Configuration in US Lab

S126E008414 - STS-126 - WRS Configuration in US Lab

S126E008424 - STS-126 - WRS Configuration in US Lab

S126E008411 - STS-126 - WRS Configuration in US Lab

S126E008387 - STS-126 - WRS Configuration in US Lab

S126E008402 - STS-126 - WRS Configuration in US Lab

S126E008394 - STS-126 - WRS Configuration in US Lab

S126E008397 - STS-126 - WRS Configuration in US Lab

S126E008439 - STS-126 - WRS Configuration in US Lab

description

Summary

The original finding aid described this as:

Description: View of umbilicals and connectors on the Water Recovery System 2 (WRS2) rack in the U.S. Laboratory / Destiny module. Image was taken during Expedition 18 / STS-126 joint operations.

Subject Terms: STS-126, Expedition Eighteen, Destiny Laboratory Module, Water Reclamation, Racks (Frames), Connectors

Date Taken: 11/19/2008

Categories: Station Configuration

Interior_Exterior: Interior

Ground_Orbit: On-orbit

Element: U.S. Laboratory

Original: Digital Still

Preservation File Format: TIFF

STS-126

Nothing Found.

label_outline

Tags

wrs configuration wrs configuration lab sts 126 endeavour nasa high resolution ultra high resolution sts 126 laboratory destiny laboratory module tiff sts 126 connectors water recovery system destiny module station configuration water reclamation expedition eighteen preservation file format expedition space program
date_range

Date

2008
create

Source

The U.S. National Archives
link

Link

https://catalog.archives.gov/
copyright

Copyright info

No known copyright restrictions

label_outline Explore Wrs Configuration, Wrs, Water Recovery System

20 INCH FAN ENGINE MODEL BELLMOUTH CONFIGURATION - ACOUSTIC MUFFLER

CONFIGURATION AND INSTALLATION OF 5.5 INCH SONIC INLET IN THE 9X15 FOOT WIND TUNNEL

J-85 F-106 AIRPLANE SPIKE INLET 40-60 TAKE OFF CONFIGURATION AT HANGAR APRON QUIET ENGINE SITE

S126E008423 - STS-126 - WRS Configuration in US Lab

GENERAL ELECTRIC GE AND BB&N TEST CONFIGURATION INST SCOOP AND MICROPHONE BOOM ARRAY

S126E008990 - STS-126 - WRS Activation in the US Lab

An F-4 Phantom II aircraft shows one angle of its weapon configuration while atop a pedestal at the Rome Air Development Center's Newport test site. The aircraft's antennas are being evaluated during the test

Under the goals of the Vision for Space Exploration, Ares I is a chief component of the cost-effective space transportation infrastructure being developed by NASA's Constellation Program. This transportation system will safely and reliably carry human explorers back to the moon, and then onward to Mars and other destinations in the solar system. The Ares I effort includes multiple project element teams at NASA centers and contract organizations around the nation, and is managed by the Exploration Launch Projects Office at NASA's Marshall Space Flight Center (MFSC). ATK Launch Systems near Brigham City, Utah, is the prime contractor for the first stage booster. ATK's subcontractor, United Space Alliance of Houston, is designing, developing and testing the parachutes at its facilities at NASA's Kennedy Space Center in Florida. NASA's Johnson Space Center in Houston hosts the Constellation Program and Orion Crew Capsule Project Office and provides test instrumentation and support personnel. Together, these teams are developing vehicle hardware, evolving proven technologies, and testing components and systems. Their work builds on powerful, reliable space shuttle propulsion elements and nearly a half-century of NASA space flight experience and technological advances. Ares I is an inline, two-stage rocket configuration topped by the Crew Exploration Vehicle, its service module, and a launch abort system. This HD video image depicts friction stir welding used in manufacturing aluminum panels that will fabricate the Ares I upper stage barrel. The aluminum panels are subjected to confidence panel tests during which the bent aluminum is stressed to breaking point and thoroughly examined. The panels are manufactured by AMRO Manufacturing located in El Monte, California. (Highest resolution available) n/a

S126E008432 - STS-126 - WRS Configuration in US Lab

S126E010905 - STS-126 - WRS Troubleshooting in US Lab, Part 2

S126E008973 - STS-126 - PWD Hose Routing in the US Lab

VANDENBERG AIR FORCE BASE, Calif. – In the Astrotech payload processing facility on Vandenberg Air Force Base in California, technicians enclose a transportation canister containing NASA's Soil Moisture Active Passive, or SMAP, spacecraft in an environmentally protective wrap for its move to the launch pad. SMAP will launch on a United Launch Alliance Delta II 7320 configuration vehicle featuring a United Launch Alliance first stage booster powered by an Aerojet Rocketdyne RS-27A main engine and three Alliant Techsystems, or ATK, strap-on solid rocket motors. Once on station in Earth orbit, SMAP will provide global measurements of soil moisture and its freeze/thaw state. These measurements will be used to enhance understanding of processes that link the water, energy and carbon cycles, and to extend the capabilities of weather and climate prediction models. SMAP data also will be used to quantify net carbon flux in boreal landscapes and to develop improved flood prediction and drought monitoring capabilities. Launch from Space Launch Complex 2 is targeted for Jan. 29. To learn more about SMAP, visit http://www.nasa.gov/smap. Photo credit: NASA/U.S. Air Force Photo Squadron KSC-2015-1090

Topics

wrs configuration wrs configuration lab sts 126 endeavour nasa high resolution ultra high resolution sts 126 laboratory destiny laboratory module tiff sts 126 connectors water recovery system destiny module station configuration water reclamation expedition eighteen preservation file format expedition space program