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SBC: MESA PHOTONICS LLC Topic: T601
Mesa Photonics, in collaboration with the College of Optics and Photonics (CREOL) at the University of Central Florida, proposes to develop a spacesuit gas sensor based upon its Enhanced Raman Gas Sensor (ERGS) technology. The goal a moisture tolerant, drop-in replacement for the current CO2 sensor. Preliminary work achieved detection sensitivities for CO2, CH4, O2, and N2 of 1000, 300, 1000 and 1 ...STTR Phase I 2015 National Aeronautics and Space Administration
SBC: OPTO-KNOWLEDGE SYSTEMS INC Topic: T801
We propose to develop and demonstrate a new sensor platform for isotope and trace-gas analysis that is appropriate for future planetary missions. Among other applications, the technology can enable the collection of isotope ratio data in support of the search for evidence of life within the solar system. Current limitations to in-situ isotope measurements will be overcome by utilizing a capillar ...STTR Phase II 2015 National Aeronautics and Space Administration
SBC: IOP Technologies LLC Topic: T603
NASA recognizes the importance of conservation, smart utilization and reuse of resources for their deep space missions to address the need for regeneration of air, water and waste with highly reliable systems to reduce mission payload. Additionally, energy for life support and other systems needs to be obtained from renewable energy sources or waste streams. In order to address NASA's requirements ...STTR Phase I 2016 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: VERAPHOTONICS INC Topic: T1201
Pressurized systems and pressure vessels used in NASA ground-based and flight-based applications including fuel tanks, composite overwrapped pressure vessels (COPVs), and composite tankage commonly suffer from several types of degradation including fatigue, cracking, lack of bonding, and leakage. Veraphotonics proposes to develop a pressure vessel leak and damage detection system. In a large vesse ...STTR Phase I 2015 National Aeronautics and Space Administration
SBC: Honeybee Robotics, Ltd. Topic: T402
In Phase 2 we will develop a fully integrated, autonomous free-flying robotic system based on a commercial SkyJib quadcopter, and demonstrate flying straight and level to a target location, acquisition of rock and regolith samples, and return to the point of origin. The work plan for Phase 2 is as follows: 1. Completion of the Guidance, Navigation, Control, Vision, and Sample Acquisition subsyste ...STTR Phase II 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: PARABILIS SPACE TECHNOLOGIES INC Topic: T101
Parabilis Space Technologies, Inc. (Parabilis), in collaboration with Utah State University (USU), proposes a low cost, high performance launch vehicle upper stage using oxygen and a novel additively manufactured polymer fuel grain as propellants in response to solicitation T1.01, Affordable Nano/Micro Launch Propulsion Stages. This technology will fulfill the ever-growing mission demands of the C ...STTR Phase I 2015 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: PC KRAUSE & ASSOCIATES INC Topic: T1501
PC Krause and Associates is partnering with Purdue University, EleQuant, and GridQuant to create a hybrid modeling capability. The combination of PCKA?s extensive dynamic modeling experience, Purdue?s work in electromechanical systems analysis, and GridQuant and Elequant?s development of the HELM algorithm uniquely positions the team to create this technology. HELM is a novel algorithm that solves ...STTR Phase I 2016 National Aeronautics and Space Administration