Award Data

The goal of this SBIR Phase II proposal is to develop a web-based platform that (1) hosts a collection of micro games for cybersecurity awareness and training; (2) simplifies the development of micro games by maximizing re-use of functionality; (3) helps administrators manage and deploy micro games; and (4) helps analysts assess readiness through a suite of tools for analytics. In Phase I, we expl ...

Long-lived Venus landers require power and cooling. Heat from the roughly 64 General Purpose Heat Source (GPHS) modules must be delivered to the convertor with minimal ÄT. The cooling system must be shutoff during the transit to Venus without overheating the GPHS modules. This program will develop an alkali metal Variable Conductance Heat Pipe (VCHP) integrated with a two-phase heat collection/tr ...

Loop heat pipes (LHPs) can provide variable thermal conductance needed to maintain electronics and batteries on Lunar/Martian rovers/landers within desired temperature range. During lunar day, the LHP transfers the heat to the radiator for rejection. During the fourteen-day-long lunar night, the sink temperature drops, lowering LHP and WEB/battery temperatures. Without a variable thermal link, the ...

This Phase I Small Business Innovative Research project proposes to develop a multiscale computational methodology capable of accurate prediction of the properties and performance of insulating ablative materials that are used to protect the re-entry of vehicles from excessive thermal loads. In particular, this effort will focus on multi-million atom, reactive molecular dynamics (MD) simulations o ...

The Full Authority Digital Engine Control (FADEC) controls engine operation. The FADEC case must be maintained below 63°C, while the environment can be as hot as 170°C. The current design uses fuel to cool the FADEC, however, this often limits the allowable ground or flight idle time before the fuel is too hot to cool the FADEC. This SBIR Phase I project will develop a thermal management syst ...

Pyrolysis processing can be used in near term missions for volume reduction, water recovery (drying), stabilization, and enhanced water and oxygen recovery through thermochemical reactions. For longer term missions, the added benefits include production of fuel, multi-purpose carbon, and reactants for in-situ resource utilization (ISRU). The objective of the Phase I SBIR program was to demonstrate ...

The Air Force is seeking new technology that will provide the means to accurately measure and monitor turbine inlet gas temperature in gas turbine engines, particularly in advanced engines operating at very high temperatures (>3,100 degree F). In Phase I of this program, Advanced Fuel Research, Inc. demonstrated that turbine inlet gas temperature can be determined from non-intrusive measurements ...

PI at ArkLight proposes a novel approach to photon counting detectors at near-IR (1-1.8 µm) and mid-IR (3-4 µm) with single photon sensitivity, representing an innovative Lidar technology for ASCENDS mission. She will convert the input signals at 1.27 µm and 1.57 µm to those at 579 nm and 634 nm, respectively, within a periodically-poled LiNbO3 wafer, pumped by a Nd:YAG laser at 1.064 µm or a ...

Today’s head-mounted displays fall short of providing wide-FOV imagery with high visual acuity. One reason for this is the difficulty of creating lightweight, distortion-free wide-angle optics. Instead of attempting to recreate the entire visual field at high resolution, we propose to present a small, high-resolution foveal image to one eye and a larger, lower-acuity peripheral image to the ot ...

High temperature piezoelectric crystal (HTPC) sensors are desired for future propulsion component structure health monitoring, operating parameters optimization, turbine engine control and health monitoring, as well as improving performance and maintainability of power production facilities and other rotary combustion engines. Recently discovered high temperature piezoelectrics showed stable piezo ...