Combustion Integrated Rack (CIR)

Combustion Integrated Rack (CIR)

Combustion Integrated Rack (CIR)

NASA, Lockheed Martin S-3B Viking Aircraft #N601NA, Unmanned Aircraft Communications Project

Lockheed S-3B Viking, N601NA at Sunrise on the Glenn Research Center Hangar Apron

Pictured is the Communications room in the RAC building, Research Analysis Center. This is the hub for the CATV and Lynk system and also the telephone system as seen from the twisted pair wires. The test gear LAN 450 is on the floor and is a spectrum analyzer made specifically for CATV. The Large boxes on the wall are Trunk amps and the smaller boxes are Splitters or combiners.

Combustion Integrated Rack (CIR)

NASA, Lockheed Martin S-3B Viking Aircraft #N601NA, Unmanned Aircraft Communications Project

Orion Capsule and Launch Abort System (LAS) installed in the NASA Glenn 8x6 Supersonic Wind Tunnel for testing. This test is an Aero Acoustic test of the LAS. Pictured is the calibration of the model's angle of attack

Advanced Colloids Experiment, Thermal 5-2, ACE T5-2 International Space Station, ISS, Fluids Integrated Rack, FIR Operations in the Telescience Support Center, TSC

Technicians ready a single rotating propeller model in the 8x6 Supersonic Wind Tunnel