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SBC: ACES QC, LC Topic: AF09BT40
The objective of Phase I is to identify the strengths and weaknesses of the various multi-reference coupled-cluster (MRCC) methods that have been proposed for the description of molecular states depending upon near degeneracies and non-dynamic electron correlation. Such effects are encountered in bond breaking, at transition states, for complex open shell systems like transition metal atoms, and f ...STTR Phase I 2010 Department of DefenseAir Force
SBC: Kassoy Innovative Science Solutions Topic: AF09BT38
Quantitative predictions of reactive flow dynamics from large-scale simulations of Liquid Rocket Engines (LRE) appear to be model dependent. Relationships and coupling among the dominant mechanisms most responsible for destabilization are obscured by the complexities of the model and subtle consequences of inherent ad hoc approximations not supported by mathematical rationale. The reliability of ...STTR Phase I 2010 Department of DefenseAir Force
SBC: TECH-X CORPORATION Topic: AF09BT10
We propose to develop a commercial weakly ionized plasma modeling capability based off of Tech-X’s high energy density plasma fluid code TxFluids. The new additions will be able to be used to model hypersonic vehicle physics including shock waves, plasma chemistry and innovative techniques for blackout mitigation and hypersonic vehicle control through the application of electric and/or magnetic ...STTR Phase I 2010 Department of DefenseAir Force
SBC: ITN ENERGY SYSTEMS, INC. Topic: AF09BT33
This Small Business Technology Transfer Research phase I program will develop a new class of uncooled THz detectors for the 1-10THz band with a novel design using surface plasmon resonant cavities with integrated metal-insulator-metal tunneling diodes as the detecting element. Tunneling diodes provide ultrafast broadband response, potentially into the visible (300THz), but demonstrated performanc ...STTR Phase I 2010 Department of DefenseAir Force
SBC: Apolent Corporation Topic: AF09BT06
We apply the theory of partially observable Markov decision processes (POMDPs) to the design of guidance algorithms for controlling the motion of unmanned aerial vehicles (UAVs) with on-board sensors for tracking multiple ground targets. While POMDPs are intractable to optimize exactly, principled approximation methods can be devised based on Bellman’s principle. We introduce a new approximation ...STTR Phase I 2010 Department of DefenseAir Force
SBC: MATHEMATICAL SYSTEMS & SOLUTIONS, INC. Topic: AF09BT13
The present text proposes development of efficient, accurate and rapidly-convergent algorithms for the simulation of propagation and scattering of electromagnetic fields within and around structures that (i) Consist of complex combinations of penetrable materials as well as perfect and imperfect conductors, and, (ii) Possess complex geometrical characteristics, including open surfaces, metallic c ...STTR Phase I 2010 Department of DefenseAir Force
SBC: OPTOMEC, INC. Topic: AF09BT26
Aerosol Jet printing is proposed as a method for printing large area, CNT-based transistor arrays on flexible substrate. The teaming relationship combines expertise in high resolution printing along with device and materials expertise. All semiconductor, dielectric, and conductive materials comprising the TFTs will be solution processed and printed with a single machine. This will lead to a cos ...STTR Phase I 2010 Department of DefenseAir Force
SBC: HPS Simulations Topic: AF09BT31
Existing computer combat wargames offer a sophisticated and high fidelity base platform for accurately modeling standard combat scenarios. However, the rapid development of UAV capabilities in terms of sizes, weapons, sensors, communications and flight ability is presenting a new challenge for these simulations. At the same time, the general state of world affairs is changing such that the likeli ...STTR Phase I 2010 Department of DefenseAir Force
Theoretical Innovations in Combining Analytical, Experimental, and Computational Combustion Stability AnalysisSBC: HYPERCOMP INC Topic: AF09BT38
Combustion stability is an important consideration in the design of liquid rocket engines. While fundamental modes of unstable operation in simple geometries are easily identified using analytical methods, recent times have seen these methods greatly expand in scope, applied in semi-numerical format to increasingly complex geometries and flow situations. Much remains to be explored in understandin ...STTR Phase I 2010 Department of DefenseAir Force
SBC: Soraa Topic: AF08BT20
We propose to demonstrate and advance several key aspects of our novel, scalable ammonothermal technology for growth of high quality single crystal gallium nitride. Specifically, we propose to demonstrate a high growth rate and high crystalline quality, to design and analyze a pilot-scale reactor, and to construct and validate a quantitative model to describe the fluid dynamics of the growth envi ...STTR Phase II 2010 Department of DefenseAir Force