Currently an important unsolved problem ferroelectric liquid crystal micro-displays in the space helmets is the annealing of dislocations generated when the smectic layers are formed on the transparent viewing screen of the display unit. The proposed liquid crystal bubble experiments resolve the annealing dislocation problem of smectic ferroelectric liquid crystal micro-displays, one of the key aspects of generating well aligned electro-optic devices. It will improve the contrast, resolution and response time of the liquid crystal display devices that are currently used on the Helmet Mounted and Head Up display systems.
• The OASIS flight instrument will be designed to interface and operate within the Microgravity Science Glovebox (MSG).
• OASIS will be designed for autonomous operation through scripts and ground commanding. Crew time is required for initial installation, checking sample loading and bubble/island formation.
• OASIS consists of seven (8) main hardware components: the Bubble Chamber Enclosure, the Bubble Chamber Insert, the Optics/Illumination Assembly, the Macro Camera, the Electronics/Power Assembly, the Avionics Assembly, Soft Start Assembly and the Digital I/O Cube Assembly.
The OASIS Experiment Module contains four (4) air jets which also contain electrodes (on two air jets) and a heater/cooler tandem (on the other two air jets), a water/glycerol injector, macro and micro cameras, and heater banks to manipulate the islands. The Data Acquisition and Control Unit (DACU) will control the experiment via ISS OASIS laptop and perform data storage.
The OASIS Experiment Module above details two views of the assembly. On the right, the MSG GN2 (Gaseous Nitrogen) line is shown at the lower left of the assembly. The air jets, illuminating white light LED panels, and bubble chamber are shown with the external housing semi-transparent for clarity. In the assembly on the right hand side, a closer view of the bubble chamber shows the injector and macro view camera.