Award Data

Alameda Applied Sciences Corporation has demonstrated the feasibility of a new type of electric propulsion device dubbed the Magnetically Enhanced Vacuum Arc Thruster (MVAT). This thruster is itself a variant on the Vacuum Arc Thruster that has been demonstrated via a recently concluded Phase I SBIR contracts from NASA. The VAT was verified to be a throttleable low mass (ca. 150g) high efficiency ...

The purpose of this Phase-I is to demonstrate the feasibility of using Alameda Applied Sciences Corporation's Coaxial Energetic Deposition (CED) process to increase the life of gun barrels, specifically the Mk-46 and Mk-48 light-weight machine guns, by depositing a protective refractory metal coating to the inside of the barrel as a replacement for the chrome coatings that are presently used. The ...

3DGeo will implement a graphical user interface (GUI) built on top of the Globus Toolkit 3.0 (GT3) middleware and complying with the Open Grid Services Infrastructure (OGSI) standard. This GUI will be a convenient interface for computational resource discovery, computational resource monitoring, and workflow submission to the Grid. These features will be built into 3DGeo?s Java-based INSP system - ...

The purpose of this program is to develop a compact and efficient ultraviolet laser system for ozone sensing from space. The basis for this system will be a diode-pumped neodymium-yttria (Nd:Y2O3) laser which is frequency-tripled to generate uv light at either 305nm or 315nm. The ability to generate both uv wavelengths from a single frequency-tripled Nd:Y2O3 laser makes this approach potentially 4 ...

The purpose of this program is to develop a compact and efficient ultraviolet laser for use in space-based uv-Raman instruments. The basis for this system will be a diode-pumped neodymium-yttria (Nd:Y2O3) ceramic laser which is frequency-quadrupled to generate uv light at 237nm. The unique combination of a low-cost and robust ceramic laser with efficient 4th harmonic generation will provide an ide ...

The ability to quickly estimate flight vehicle behavior in an operational environment is important since engineers from a variety of disciplines require accurate predictions in order to plan flight test experiments, expand aircraft operating envelopes safely, and have access to diagnostic methods when problems arise. STARS is the most comprehensive multidisciplinary finite element-based software f ...

The NASA objective of expanding the human experience into the far reaches of space will require the development of regenerable life support systems. On-board carbon dioxide (CO2) removal units play a key role in such systems ensuring high quality cabin air for crew members. Similar but more compact units are needed for extravehicular activities (space suit). The overall objective is to develop ...

The objective of the Phase I SBIR program was to demonstrate the feasibility of integrating pyrolysis and incineration steps into a system for processing of spacecraft solid wastes. The Phase I study involved a combination of bench scale experiments and data analysis. This work was accomplished in four tasks: 1) design and construct bench scale unit; 2) laboratory studies on solid waste processing ...

This Phase I project will demonstrate the feasibility of providing panoramic stereoscopic images for remote-controlled robotic space operations using three fixed-position cameras. Remote-controlled robot operations are an important element in orbital and planetary space missions. Advanced display systems can greatly enhance the effectiveness of these operations. In the system proposed here, hum ...

The objective of the proposed Phase II effort is to transfer proven sensor technology from the laboratory breadboard to a functional flight-ready prototype for installation in an aircraft fuel tank. In the Phase I effort, a novel spectroscopic technique was shown to be an effective method for measuring oxygen concentration in harsh environments with sufficient accuracy for use in an OBIGGS system. ...