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LASER ANEMOMETER SYSTEM IN TEST CELL W-8 IN THE COMPRESSORS AND TURBINE C&T WING - HIGH TEMPERATURE INSTRUMENT FLOW STAND IN TEST CELL CE-13 IN THE ENGINE RESEARCH BUILDING ERB

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Summary

The original finding aid described this as:

Capture Date: 2/6/1979

Keywords: Larsen Scan

Location Building No: 0

Location Room: W-8 & CE-13

Photographs Relating to Agency Activities, Facilities and Personnel

Nothing Found.

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laser anemometer system laser anemometer system test cell test cell w compressors turbine c and t wing turbine c and t wing high temperature instrument flow high temperature instrument flow ce test cell ce engine research building erb nasa national aeronautics and space administration high resolution ultra high resolution workers industrial history space program 1970 s us national archives
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Date

1979
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The U.S. National Archives
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https://catalog.archives.gov/
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label_outline Explore Test Cell Ce, Test Cell W, Turbine C And T Wing

The new air compressors which furnish power to drive the drills, about 500 feet below the surface of the earth.

ENGINE RESEARCH BUILDING ERB CENTER SECTION EQUIPMENT

FIRE INVESTIGATION IN TEST CELLS W-2 AND W-4 IN THE COMPRESSOR AND TURBINE C&T WING OF THE ENGINE RESEARCH BUILDING ERB

ERB ENGINE RESEARCH BUILDING COMBUSTION AIR DRYER

NASA NBS CALORIMETERS IN LASER LABORATORY

Aluminum casting. Shelf after shelf of aluminum castings on their way to the heat treating oven for low temperature precipitation treatment. These castings are for aluminum piston heads. Aluminum Industries Inc., Cincinnati, Ohio

MARGARET HALLE IN THE ENGINE RESEARCH BUILDING ERB LUNCH ROOM - ERBROOM

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, United Space Alliance worker Dan Kenna (right) positions a Reinforced Carbon Carbon panel on the table to perform flash thermography. In the background, Paul Ogletree observes the monitor. Attached to the leading edge of the wing of the orbiters, the gray carbon composite RCC panels have sufficient strength to withstand the aerodynamic forces experienced during launch and reentry, which can reach as high as 800 pounds per square foot. The operating range of RCC is from minus 250º F to about 3,000º F, the temperature produced by friction with the atmosphere during reentry.

HIGH PRESSURE FACILITY HPF COMPRESSORS 1 AND 2 AND TURBINE RIG

TEST ARTICLE CONFIGURATIONS IN TEST CELL 13 IN THE OLD ROCKET LABORATORY ORL

FIRE INVESTIGATION IN TEST CELLS W-2 AND W-4 IN THE COMPRESSOR AND TURBINE C&T WING OF THE ENGINE RESEARCH BUILDING ERB

TEST CELL CE-5B IN THE ENGINE RESEARCH BUILDING ERB

Topics

laser anemometer system laser anemometer system test cell test cell w compressors turbine c and t wing turbine c and t wing high temperature instrument flow high temperature instrument flow ce test cell ce engine research building erb nasa national aeronautics and space administration high resolution ultra high resolution workers industrial history space program 1970 s us national archives