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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

GRC-2007-C-02472

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

Curtis Flack (left) and Paul von Hardenberg (right) inspect the ice formation on the spinner of an Advanced Air Mobility proprotor model tested in the Icing Research Tunnel. The data from the test will be used by icing researchers to better understand the risks of icing on electric vertical takeoff and landing vehicles which will assist with the design and certification of new aircraft.

AAM Rotor Icing Evaluation Studies (AIRES) I Test Documentation Photos at the Icing Research Tunnel (IRT)

Curtis Flack (left) and Paul von Hardenberg (right) inspect the ice formation on the spinner of an Advanced Air Mobility proprotor model tested in the Icing Research Tunnel. The data from the test will be used by icing researchers to better understand the risks of icing on electric vertical takeoff and landing vehicles which will assist with the design and certification of new aircraft.