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SBC: GLOYER-TAYLOR LABORATORIES INC Topic: T1201
GTL?s SNS technology aids in the operation of new or existing structural health monitoring (SHM) systems by integrating data and power pathways into the structure. The use of this technology within a composite structure would allow engineers to place sensors from an SHM system directly where they are needed on a structure with instant power. GTL?s SNS technology offers the potential for developers ...STTR Phase I 2016 National Aeronautics and Space Administration
SBC: HJ SCIENCE & TECHNOLOGY INC Topic: T803
HJ Science & Technology (HJS&T) and Georgia Institute of Technology (GIT) propose to develop a novel penetrator-compatible technology capable of detecting key organic molecules, biomarkers, and indicators of habitability on primary astrobiological targets including icy moons like Europa and Enceladus. The proposed innovation is a novel combination of microfluidic automated colorimetric and fluo ...STTR Phase I 2016 National Aeronautics and Space Administration
SBC: GLOYER-TAYLOR LABORATORIES INC Topic: T101
The proposed technology builds off GTL's advanced solid ramjet fuel. The method uses additive manufacturing methods to produce an innovative new type of fuel grain that regresses quickly and has a high Isp and combustion efficiency. With this technology, the performance of a liquid rocket engine can be had with a hybrid rocket system. This technology allows for a simple, low cost, high performanc ...STTR Phase I 2015 National Aeronautics and Space Administration
SBC: PREDICTIVE SCIENCE INCORPORATED Topic: T602
Solar Particle Events (SPEs) represent a major hazard for extravehicular maneuvers by astronauts in Earth orbit, and for eventual manned interplanetary space travel. They can also harm aircraft avionics, communication and navigation. We propose to develop a system to aid forecasters in the prediction of such events, and in the identification/lengthening of "all clear" time periods when there is a ...STTR Phase I 2015 National Aeronautics and Space Administration
Gust Load Estimation and Rejection With Application to Robust Flight Control Design for HALE AircraftSBC: Systems Technology, Inc. Topic: T401
High Altitude Long Endurance (HALE) aircraft have garnered increased interest in recent years as they can serve several purposes, including many of the objectives of satellites while incurring a fraction of the cost to deploy. Examples applications include Intelligence, Surveillance, and Reconnaissance, communications relay systems, and environmental and atmospheric sensing. The requirements for H ...STTR Phase I 2015 National Aeronautics and Space Administration
SBC: Linked, Inc. Topic: T401
The objective of this proposed project is to provide a new set of sensitivity analysis theory and codes, the Sensitivity Analysis for Design Optimization Integrated Software Tool set, to work within the existing NASA O3 Tool. In this Phase I effort, the sensitivity approach will be implemented for two basic types of analysis, namely static systems of equations (linear and non-linear) and eigen-pro ...STTR Phase I 2016 National Aeronautics and Space Administration
SBC: VERAPHOTONICS INC Topic: T1201
Pressurized systems and pressure vessels used in NASA ground-based and flight-based applications including fuel tanks, composite overwrapped pressure vessels (COPVs), and composite tankage commonly suffer from several types of degradation including fatigue, cracking, lack of bonding, and leakage. Veraphotonics proposes to develop a pressure vessel leak and damage detection system. In a large vesse ...STTR Phase I 2015 National Aeronautics and Space Administration
SBC: GLOYER-TAYLOR LABORATORIES INC Topic: T301
DEC-Shield technology offers the means to generate electric power from cosmic radiation sources and fuse dissimilar systems and functionality into a structural component to create a Multi-functional Structure (MFS). DEC-Shield integrated into MFS technology can be used to generate electric power and provide radiation protection in a space vehicle; even maximizing that protection by spreading the ...STTR Phase I 2016 National Aeronautics and Space Administration
SBC: CFD RESEARCH CORPORATION Topic: T102
Chemical contamination of spacecraft components as well as thermal and force loading from firing liquid propellant thrusters are critical concerns for in-space propulsion applications. Gas molecular contamination and liquid droplet deposition due to incomplete combustion threaten to damage surface materials, sensitive instruments and optical sensors, and poses major risks for mission success. Liqu ...STTR Phase I 2016 National Aeronautics and Space Administration
SBC: MESA PHOTONICS LLC Topic: T601
Mesa Photonics, in collaboration with the College of Optics and Photonics (CREOL) at the University of Central Florida, proposes to develop a spacesuit gas sensor based upon its Enhanced Raman Gas Sensor (ERGS) technology. The goal a moisture tolerant, drop-in replacement for the current CO2 sensor. Preliminary work achieved detection sensitivities for CO2, CH4, O2, and N2 of 1000, 300, 1000 and 1 ...STTR Phase I 2015 National Aeronautics and Space Administration