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SBC: M4 ENGINEERING, INC. Topic: T401
In aircraft design, reducing structural weight is often a prime objective, while various constraints in multiple disciplines, such as structure, aerodynamics and aeroelasticity should be imposed on the aircraft. Therefore, engineers need optimization tools to incorporate the multidisciplinary constraints using appropriate fidelity during the early stages of concept design. Classic structural desi ...STTR Phase II 2015 National Aeronautics and Space Administration
SBC: ATA ENGINEERING, INC. Topic: T1201
ATA Engineering, Inc. proposes an STTR program to develop innovative tools and methods that will significantly improve the accuracy of random vibration response predictions for aerospace structures under critical inhomogeneous aeroacoustic loads. This will allow more accurate predictions of structural responses to be made, potentially reducing vehicle weight and cost and improving the reliability ...STTR Phase II 2015 National Aeronautics and Space Administration
SBC: GLOYER-TAYLOR LABORATORIES INC Topic: T102
GTL has been developing a suite of transformational technologies that have the capability to disrupt the traditional launch vehicle paradigm. BHL composite cryotank technology provides a four times improvement over large aluminum iso-grid tanks, offering a 6 percentage point improvement in small stage PMF. Superior Stability Engine is an innovative liquid rocket engine configured to maximize comb ...STTR Phase II 2015 National Aeronautics and Space Administration
SBC: CFD RESEARCH CORPORATION Topic: T1204
Despite the rapid commercialization of additive manufacturing technology such as selective laser melting, SLM, there are gaps in process modeling and material property prediction that contribute to slow and costly process development, process qualification and product certification. To address these gaps, CFDRC and our partner Dr. Kevin Chou, University of Alabama, will develop multiple computatio ...STTR Phase II 2015 National Aeronautics and Space Administration
Infectious Disease Diagnostics and Differentiation of Viral vs. Bacterial Infections for Point of Care ApplicationsSBC: GENECAPTURE, INC. Topic: CBD15C001
The modern warfighter faces the constant threat of endemic infections, multi-drug resistant bacteria and Biological Warfare Agents. In order to provide accurate front-line treatment that will curtail the overuse of antibiotics, a rapid and robust moleculaSTTR Phase I 2016 Department of DefenseOffice for Chemical and Biological Defense
SBC: BLUECOM SYSTEMS & CONSULTING LLC Topic: T501
There is growing recognition that success in a variety of space mission types can be greatly enhanced by making current communication transceivers and networks evolve towards networked communication systems that are intelligent, self-aware and thus can support greater levels of autonomy. This will be especially relevant as networked clusters of smaller-size satellites, made of CubeSats or microsat ...STTR Phase I 2015 National Aeronautics and Space Administration
Integrated Reacting Fluid Dynamics and Predictive Materials Degradation Models for Propulsion System ConditionsSBC: CFD RESEARCH CORPORATION Topic: T1202
Computational fluid dynamics (CFD) simulations are routinely used by NASA to optimize the design of propulsion systems. Current methods for CFD modeling rely on general materials properties to determine fluid structure interactions. This introduces uncertainty when modeling extreme conditions, where materials degrade and properties may change as a consequence. This also limits the use of CFD as a ...STTR Phase I 2015 National Aeronautics and Space Administration
SBC: Space Micro Inc. Topic: T501
Space Micro and its partner research institution, the University of Arizona bring together innovations in channelization and network protocol development. Together, these innovations will provide improved hopping radios (with digital, rapidly reconfigurable implementation, wider bandwidth and reduced overhead penalty for hopping) and improved spectrum and link quality sensing. We will demonstrate ...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: M4 ENGINEERING, INC. Topic: T401
We propose the development of a modern panel code for calculation of steady and unsteady aerodynamic loads needed for dynamic servoelastic (DSE) analysis of flight vehicles. The code will be especially tailored to be robust, reliable, and integrated with the NASA Object Oriented Optimization (O3) system through selection of analysis methods, file formats, and computing environment, allowing it to ...STTR Phase I 2015 National Aeronautics and Space Administration