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SBC: NANOSONIC INC. Topic: T1203
Future long-duration, crewed space habitat systems will be inflatable structures. This type of structure is advantageous in that it is not limited to the diameter of the launch vehicle and can therefore provide a greater volume of living and work space. Unlike conventional metal structures, however, softbody inflatables require support members to maintain their desired shapes. Despite their robust ...STTR Phase I 2016 National Aeronautics and Space Administration
SBC: TDA RESEARCH, INC. Topic: T604
TDA Research Inc.(TDA) in collaboration with University of Puerto Rico ? Mayaguez (UPRM is proposing to develop a highly efficient CO2 removal system based on UPRM proprietary strontium exchanged silico-alumino-phosphate (Sr-SAPO-34) for closed loop space craft cabin air re-vitalization during deep space missions.STTR Phase I 2016 National Aeronautics and Space Administration
Metal Digital Direct Manufacturing (MDDM) for Close-Out of Combustion Chambers and Nozzle FabricationsSBC: Keystone Synergistic Enterprises, LLC Topic: T1204
This NASA sponsored STTR project will investigate methods for close-out of large, liquid rocket engine, nickel or stainless steel nozzle, coolant channels utilizing robotic laser and pulsed-arc additive manufacturing (AM)methods. Structural jacket to coolant channel land area interface strength will be quantified and metallurgical characterization completed. Process optimizations will be conducte ...STTR Phase II 2017 National Aeronautics and Space Administration
SBC: Radiometrics Corporation Topic: T103
Launch safety and efficiency requires timely and accurate wind, thermodynamic and pressure information from the surface to 20 km height, and lightning risk identification. A Doppler radar now provides wind measurements that satisfy this requirement at the Eastern Test Range. Thermodynamic soundings are provided by intermittent radiosondes on launch day. Typical intervals of an hour or more between ...STTR Phase I 2017 National Aeronautics and Space Administration
SBC: EMBEDDED DYNAMICS LLC Topic: T1501
The tiltwing class of aircraft consists of vehicles with the ability to rotate the wing and propulsion system as a unit a full 90 degrees from the standard fixed wing configuration to one in which the wing and thrust axis become perpendicular to the body axis. This thrust vectoring capability allows the aircraft to utilize thrust borne flight for vertical takeoff and landing as well as the convent ...STTR Phase I 2017 National Aeronautics and Space Administration
SBC: Luna Innovations Incorporated Topic: T802
Luna will team with Dr. John Bowers of UCSB to develop an Optical Frequency Domain Reflectometry (OFDR) system-on-chip using heterogeneous silicon photonics to enable a minimal weight structural health monitoring system. This system-on-chip will be the building block for distributed sensing interrogation systems that are the size of a deck of playing cards. This lightweight, rugged, and miniature ...STTR Phase I 2017 National Aeronautics and Space Administration
SBC: Universal Technology Corporaration Topic: T1204
In this Phase II STTR project, the proposed collaborative effort between UTC, AFIT, and ULRF represents a crucial step forward for AM. UTC’s unique AM optimization and process control framework, constructed entirely from experimental sensor data collected in-situ, will finally transfer technology from our SLM test bed system to state-of-the-art and commercial-grade systems, including a Concept ...STTR Phase II 2017 National Aeronautics and Space Administration
SBC: Advanced Systems/Supportability Engineering Technologies And Tools, Inc. Topic: N05149
The S-351 mini-sub is a prototype of the Dry Combat Submersible (DCS). This prototype was established as a means of risk reduction prior to a full commitment to the DCS program. Both of these platforms have an operational need to transit with minimum operator fatigue safely to a pre-defined point and covertly deploy and retrieve SEALS. To meet these operational needs, these platforms require upgra ...STTR Phase II 2017 Department of DefenseSpecial Operations Command
SBC: Luna Innovations Incorporated Topic: T1202
Polymer matrix composites are increasingly replacing traditional metallic materials in NASA launch vehicles. However, the repair and subsequent inspection methods for these materials are considerably more complicated. Typically, a composite laminate patch must be manually fabricated and bonded or co-cured to the damaged structure. To ensure high quality patches with sufficient compaction and l ...STTR Phase I 2017 National Aeronautics and Space Administration
SBC: LASER & PLASMA TECHNOLOGIES LLC Topic: T801
Laser & Plasma Technologies (LPT), teamed with the National Science Foundation (NSF) Center for Lasers at the University of Virginia (UVA), proposes an advanced optical fiber coupled hybrid spectroscope for in situ characterization of organic compounds. The proposed approach provides information on organic compounds by analyzing spectra obtained from Laser Induced Breakdown Spectroscopy (LIBS) an ...STTR Phase I 2017 National Aeronautics and Space Administration