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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: Honeybee Robotics, Ltd. Topic: T402
The World is Not Enough (WINE) is a new generation of CubeSats that take advantage of ISRU to explore space. The WINE takes advantage of existing CubeSat technology and combines it with 3D printing technology and an In Situ Resource utilization (ISRU) water extraction system. 3D printing enables development of steam thrusters (higher Isp than cold gas) as well as tanks that fit within the availabl ...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
SBC: CFD RESEARCH CORPORATION Topic: T102
Advanced turbomachinery components play a critical role in launch vehicle and spacecraft liquid rocket propulsion systems. To achieve desired efficiencies, extremely tight tolerances are often imposed between inducer blades and shrouds or other system components which sets up strong interactions that influence both the aerodynamics and the structural performance of blades and vanes. These transien ...STTR Phase I 2016 National Aeronautics and Space Administration
SBC: CFD RESEARCH CORPORATION Topic: T102
Chemical contamination of spacecraft components as well as thermal and force loading from firing liquid propellant thrusters are critical concerns for in-space propulsion applications. Gas molecular contamination and liquid droplet deposition due to incomplete combustion threaten to damage surface materials, sensitive instruments and optical sensors, and poses major risks for mission success. Liqu ...STTR Phase I 2016 National Aeronautics and Space Administration