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SBC: M4 ENGINEERING, INC. Topic: T401
We propose the development of a novel aerodynamic modeling approach making use of fully unstructured grids for unsteady panel aerodynamic models for aeroelastic and aeroservoelastic analysis. The unsteady aerodynamic code will be integrated with an existing suite of aeroelastic and aeroservoelastic analysis tools making it possible to perform aeroelastic and aeroservoelastic analysis of complex v ...STTR Phase II 2016 National Aeronautics and Space Administration
SBC: CHROMOLOGIC LLC Topic: T801
Chromologic (CL) and the California Institute of Technology (Caltech) propose to continue the Phase II STTR development and demonstration of a Multifunctional Environmental Digital Scanning Electron Microprobe (MEDSEM) instrument that transmits high energy beams of electrons sequentially using a two-dimensional array of multiple, miniaturized electron probes into a planetary atmosphere and strike ...STTR Phase II 2016 National Aeronautics and Space Administration
SBC: PARABILIS SPACE TECHNOLOGIES INC Topic: T101
Parabilis Space Technologies, Inc (Parabilis), in collaboration with Utah State University (USU), proposes further development of a low-cost, high-performance launch vehicle upper stage that uses a high density, storable oxidizer and a polymer fuel grain as propellants in response to solicitation T1.01, Affordable Nano/Micro Launch Propulsion Stages. This effort will build upon the successful opti ...STTR Phase II 2016 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 ...STTR Phase II 2016 National Aeronautics and Space Administration
SBC: INTELLIGENT OPTICAL SYSTEMS, INC. Topic: T601
The gas sensor in the PLSS of the ISS EMU will meet its projected life in 2020, and NASA is planning to replace it. At present, only high TRL devices based on infrared absorption are candidate replacements, because of their proven long-term stability, despite their size and power consumption and failures in the presence of liquid water. No current compact sensor has the tolerance for liquid water ...STTR Phase II 2016 National Aeronautics and Space Administration
SBC: CFD RESEARCH CORPORATION Topic: T602
High-energy space radiation from Galactic Cosmic Rays and Solar Particle Events (SPEs) pose significant risks to equipment and astronaut health in NASA missions. Energetic particles from SPEs associated with flares and coronal mass ejections (CMEs) may adversely affect not only beyond-Low-Earth-Orbit missions, but also aircraft avionics, communications, and airline crew/passenger health. It is cru ...STTR Phase II 2016 National Aeronautics and Space Administration
SBC: AMERICAN GNC CORPORATION Topic: T1301
American GNC Corporation (AGNC) and Louisiana Tech University (LaTECH) are proposing a significant breakthrough technology, the Integrated Monitoring AWAReness Environment (IM-AWARE) consisting of an Enterprise Infrastructure with closely coupled smart sensor networks and Enhanced IT Security to enable: (i) real time monitoring of the distribution systems health; (ii) supporting maintenance operat ...STTR Phase II 2016 National Aeronautics and Space Administration
An End-To-End Microfluidic Platform for Engineering Life Supporting Microbes in Space Exploration MissionsSBC: HJ SCIENCE & TECHNOLOGY INC Topic: T601
HJ Science & Technology (HJS&T) and Lawrence Berkeley National Laboratory (LBNL) propose a highly integrated, programmable, and miniaturized microfluidic automation platform capable of running rapid and complex synthetic biology and bioengineering processes for engineering life supporting microbes in space exploration missions. Our approach combines the microfluidic automation technology of HJS&T ...STTR Phase II 2015 National Aeronautics and Space Administration
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: 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