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Aviation Machinist�s Mate 3rd Class Benjamin Bonner inspects a jet fan module for defects aboard USS Kitty Hawk (CV 63).

ALTITUDE WIND TUNNEL AWT HARDWARE

Main pulse power supply after revisions. Photograph taken January 23, 1962. Bevatron-2581 – Photographer: George Kagawa

KENNEDY SPACE CENTER, FLA. -- Processing for mission STS-107 continues in the Operations and Checkout Building as the tunnel that will connect Space Shuttle Columbia's crew compartment to the SPACEHAB module is moved into a transportation canister. A research mission, the primary payload of STS-107 is the SHI Research Double Module (SHI/RDM) or SPACEHAB, making its first flight. The experiments on board will range from material sciences to life sciences (many rats). STS-107 is scheduled to launch July 19, 2002 KSC-02pd0652

ZERO GRAVITY FACILITY SHOP AREA SHOWING CROWDED CONDITIONS

S126E011389 - STS-126 - Survey of S1, S3 Trusses during Expedition 18/STS-126

KENNEDY SPACE CENTER, FLA. -- At Astrotech Space Operations, a worker prepares the THEMIS spacecraft for black/white light inspection. White light inspection assures the telemetry is operating. Black light inspection uses UVA fluorescence to detect possible particulate microcontamination, minute cracks or fluid leaks. THEMIS consists of five identical probes, the largest number of scientific satellites ever launched into orbit aboard a single rocket. This unique constellation of satellites will resolve the tantalizing mystery of what causes the spectacular sudden brightening of the aurora borealis and aurora australis - the fiery skies over the Earth's northern and southern polar regions. THEMIS is scheduled to launch Feb. 15 from Cape Canaveral Air Force Station. Photo credit: NASA/George Shelton KSC-07pd0044

STS096-361-025 - STS-096 - MS Rominger at aft flight deck controls during docking

N-231 High Reynolds Number Channel Facility (An example of a Versatile Wind Tunnel) Tunnel 1 I is a blowdown Facility that utilizes interchangeable test sections and nozzles. The facility provides experimental support for the fluid mechanics research, including experimental verification of aerodynamic computer codes and boundary-layer and airfoil studies that require high Reynolds number simulation. (Tunnel 1) ARC-1980-AC80-0512-2

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F-100 ENGINE SERIAL NO. 072 IN THE PROPULSION SYSTEMS LABORATORY PSL - DEEK THROTTLE CONTROL ROOM - DEEK SYSTEM CONTROL ROOM

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Summary

F-100 ENGINE SERIAL NO. 072 IN THE PROPULSION SYSTEMS LABORATORY PSL - DEEK THROTTLE CONTROL ROOM - DEEK SYSTEM CONTROL ROOM

NASA Identifier: C-1978-4342

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nasa f 100 engine serial no 072 in the propulsion systems laboratory psl deek throttle control room deek system control room dvids high resolution glenn research center aviation research organization
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Date

1978
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Defense Visual Information Distribution Service
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https://www.dvidshub.net/
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Public Domain Dedication. Public Use Notice of Limitations: https://www.dvidshub.net/about/copyright

label_outline Explore Aviation Research Organization, Glenn Research Center

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nasa f 100 engine serial no 072 in the propulsion systems laboratory psl deek throttle control room deek system control room dvids high resolution glenn research center aviation research organization