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3 FOOT LOW TEMPERATURE HEAT PIPE AND COMMUNICATION TECHNOLOGY SATELLITE CTS HEAT PIPE TEST FACILITY

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Summary

The original finding aid described this as:

Capture Date: 10/2/1974

Photographer: DONALD HUEBLER

Keywords: Larsen Scan

Photographs Relating to Agency Activities, Facilities and Personnel

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Tags

foot temperature heat pipe temperature heat pipe communication technology satellite cts nasa test facility national aeronautics and space administration high resolution ultra high resolution communication technology satellite cts heat pipe test facility facilities photographer donald huebler nasa photographs 1970s 1970 s space program us national archives
date_range

Date

1974
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Source

The U.S. National Archives
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Link

https://catalog.archives.gov/
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label_outline Explore Test Facility, Cts, Pipe

SMALL TEST FACILITY IN INSULATION ASSEMBLY AREA

SOLAR HEAT DRAWINGS, NASA Technology Images

COMMUNICATION TECHNOLOGY SATELLITE CTS ANTENNA FARM

COMMUNICATION TECHNOLOGY SATELLITE CTS LAUNCH

2 HIGH TEMPERATURE PRESSURE FURNACES IN THE MATERIALS AND STRESSES M&S BUILDING ROOM 31

DAMAGED HEAT EXCHANGERS, NASA Technology Images

S130E009086 - STS-130 - Node 3 Deck Alcove Internal View

8X6 FOOT WIND TUNNEL FOR LEWIS NEWS NEWSLETTER STORY ABOUT THE 30TH ANNIVERSARY

U.S. Air Force TECH. SGT. Scott Butler, a Weather Technician assigned to the 90th Fighter Squadron, Elmendorf Air Force Base, Alaska, adjusts the temperature sensor on a piece of TMQ-53 Tactical Meteorological Equipment, while deployed with the 3rd Air Expeditionary Group at Kwang-Ju Air Base, Republic of Korea on Sept. 9, 2004. (U.S. Air Force PHOTO by TECH SGT. Corey A Clements) (Released)

VENT 5-2 WITH BOUNDARY LAYER TRIP MODEL IN THE 8X6 FOOT WIND TUNNEL

Australian Coalition forces train Hostage Rescue Team

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.

Topics

foot temperature heat pipe temperature heat pipe communication technology satellite cts nasa test facility national aeronautics and space administration high resolution ultra high resolution communication technology satellite cts heat pipe test facility facilities photographer donald huebler nasa photographs 1970s 1970 s space program us national archives