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The powerful fan and motor at the heart of the Icing Research Tunnel is capable of producing continuous airspeeds up to 395 mph.
The powerful fan and motor at the heart of the Icing Research Tunnel is capable of producing continuous airspeeds up to 395 mph.

The powerful fan and motor at the heart of the Icing Research Tunnel is capable of producing continuous airspeeds up…

PFM powered force model rotor
PFM powered force model rotor

PFM powered force model rotor. This image shows one possible type of ice accretion that the Icing Tunnel can produce.

Bell 609 Spinner Inlet Icing Model
Bell 609 Spinner Inlet Icing Model

Bell 609 spinner inlet icing model. Technicians taking measurement of ice accretions after an icing test.

Technicians pose with the ERJ-170 airfoil set up for testing the IRT.
Technicians pose with the ERJ-170 airfoil set up for testing the IRT.

Technicians pose with the ERJ-170 airfoil set up for testing the IRT.

Biomedical Testing Module Serves as Home for Mice in Space
Biomedical Testing Module Serves as Home for Mice in Space

A biomedical testing module served as the home for mice in microgravity and contributed to the development of drugs to…

Lightweight, Flexible Solar Arrays are Used by Troops in Desert Regions
Lightweight, Flexible Solar Arrays are Used by Troops in Desert Regions

U.S. troops in desert regions are already using flexible, lightweight solar arrays developed by MicroLink Devices Inc., in part with…

Flexible Solar Cells Could Help Power Space Exploration
Flexible Solar Cells Could Help Power Space Exploration

Microlink Devices Inc., uses a reusable substrate to produce flexible solar cells that can be used in space and on…

F-18 tethered “free flight” model.
F-18 tethered “free flight” model.

F-18 tethered “free flight” model.

3% Blended Wing Body (BWB) – the “450” model in the 14 x 22 foot wind tunnel.
3% Blended Wing Body (BWB) – the “450” model in the 14 x 22 foot wind tunnel.

3% Blended Wing Body (BWB) – the “450” model in the 14 x 22 foot wind tunnel.

Isolated Rotor Test System in the 14 x 22 foot wind tunnel.
Isolated Rotor Test System in the 14 x 22 foot wind tunnel.

Isolated Rotor Test System in the 14 x 22 foot wind tunnel.