Award Data

We propose a rapid mapping and 3-D visualization system especially suited for inside buildings, tunnels, urban canyons, and other environments where GPS may be poor or not available. The system--which was fully demonstrated in our Phase I effort-- includes mobile Sensor Nodes that wirelessly supply compressed 3D range data and color imagery to a central Fusion Node. The Fusion Node runs 3D recon ...

The overall goal of this STTR program is to develop an efficient, high-fidelity, CFD-based design tool for the simulation of ship-board flight testing of autonomous UAV systems. In the first phase of this program, an overall flight simulation framework that employs a modular approach to the flight simulation problem was developed. Phase II of the program demonstrated a fully coupled aircraft/ship ...

To address the Navy"s need for a common, scalable, platform for multi-modal 1pA level current sensing for Electrocardiogram (ECG), Electroencephalogram (EEG), and Electrodermal Response (EDR) to be fielded as a miniature wearable device with non-contact electrodes, Sentient and the State University of New York (SUNY) propose to develop the Bioelectronic Fusion Sensor System (BioFuSenS) that will a ...

A model for structural health measurement is desired that is capable of assessing the accumulated damage and remaining useful life of components post-flight. This model will eliminate the need for load tracking during flight and prevent the additional weight and complexity of components utilized during flight. Safe is partnering with researchers at University of Memphis for this work to relate the ...

Combustion instability, or screech, occurs in many modern gas turbine systems, and is due to the complex physical coupling of the acoustic resonances in the combustion chamber with fluctuations in the heat release of the combustion process. These instabilities can produce large pressure fluctuations that can be severe enough to damage engine hardware. Next-generation gas turbines will increase the ...

Historically, aircraft engines have featured relatively simple axisymmetric exhaust shapes with several moving parts; however, future engine exhaust systems are expected feature compact, sinuous ducts with complex non-axisymmetric shapes, fixed exit areas, thrust vectoring etc., constructed with a minimum number of moving parts. Their exhaust plumes are currently not well understood; however, LES ...

Modern aircraft make extensive use of fasteners made of steel, titanium, nickel and other alloys mated with aluminum and composite airframe materials. This coupling of dissimilar materials yields galvanic corrosion issues, which degrades mechanical integrity, is costly to inspect, and poses a safety and reliability risk. Traditional design approaches of corrosion rate predictions based on open cir ...

In this project, we will develop innovative and advanced display and processing techniques, and innovatively combine existing algorithms, software, and systems, to create a Detection Avoidance System for Submarines (DASS) that assists the submarine operator, planner, and commanding officer (CO) in minimizing the probability that a submarine penetrating into and operating within an A2/AD zone will ...

Advanced effective Micro-glider development will be conceived under this Phase I effort.

We propose to develop a multi-functional coating technology using a three-component nanocomposites to achieve excellent syperhydrophobicity, anti-icing, enhanced track-resistance, and high dielectric breakdown strenght. The coating will be compatible with current Navy existing VLF device materials and be ease of applications in outdoor field, and be long lasting requiring infrequent applications.