Award Data

In this project, the development of a novel panoramic, stereoscopic video system was proposed. The proposed system, which contains no moving parts, uses three-fixed position cameras equipped with NASA's Panoramic Refracting Optic (PRO) to generate stereoscopic images over a hemispherical work area. This system will provide an immersive remote environment for robot operation during space missions ...

This project addresses two vital problems for long-term space travel activities: radiation shielding and hydrogen storage for power and propulsion. While both problems have been studied for many years, there is currently no satisfactory technology for providing adequate non-parasitic shielding. Even in low-Earth orbit, astronauts must be closely monitored for radiation exposure, and some mission ...

Advanced Technologies Group, ATG, proposes a Hybrid Advanced Robust Dependable (HARD) Seal that exceeds the Army's advanced high temperature seal application requirements. The ATG HARD seal is a non-contacting film riding seal design that will build on patented hybrid-Brush seal success at ATG. This vanguard design, when combined with advanced high temperature materials will provide unrivaled dura ...

Advanced Technologies Group, Inc. proposes the development of a Liquid-Oxygen Mass Gauge, (LMG) for In-Space cryogenic storage capable of continuous monitoring of liquid quantities to better than 1% accuracy. The proposed sensor builds on previous liquid hydrogen sensor development successes and patents. It can be utilized to measure cryogenic propellants, and sub-critical cryogenic fluids in us ...

Advanced Technologies Group, Inc. proposes the development of a Cryogenic Flow Sensor (CFS) for determining mass flow of cryogens in spacecraft propellant management. Current point sensor technology is incapable of determining high pressure, high flow rate cryogenic fluid quality and mass flow rate, and has proven to be inaccurate in attempting to rapidly measure cryogen depletion. If there is a ...

ACI proposes a design for a Propulsor (Low Cost/Low Noise Variable Pitch Ducted Fan) that has wide application in all sectors of Aviation. Propulsor hardware of this low cost design can be integrated with a broad range of aircraft engines (e.g. existing piston engines, automotive derivative piston engines, new design turbine engines) for use in new design aircraft. The proposed Propulsor desig ...

A prototype Next Generation MK III Lightweight HUT/Hatch Assembly will be fabricated and delivered during Phase II. Maximum weight reduction for the Hard Upper Torso - Hatch assembly will be acheived via the innovative material selection and cross sectional redesign investigation Air-Lock conducted during Phase I. The intent is to fabricate a lightweight HUT/Hatch Assembly best suited for space & ...

Air-Lock will deliver a final report based on the follwoing: 1. Historical summary of bearing design evolution throughout the life of the EMU Program 2. Material research to identify lightweight materials best suited for each beairng. 3. Redesign of current EMU bearings to lower bearing profile and mass.

The objective of this research is to investigate the technical feasibility of building a bidirectional converter to achieve the power density, efficiency, and coolant temperature objectives using an innovative marriage of state-of-the-art technologies. These technologies each represent innovations in their respective fields. The power electronics team at Advanced Power Electronics Corp. is prop ...

Traumatic brain injury (TBI) is a leading cause of combat casualty. Previous estimates for 20th century conflicts were that 15 - 25% of all injuries were sustained to the head. However, with the increased incidence of blast injuries that military personnel are suffering in the current conflicts in Afghanistan and Iraq, head injury is becoming an even more frequent occurrence. Far forward medics ...