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The Award database is continually updated throughout the year. As a result, data for FY19 is not expected to be complete until April, 2020.

  1. 1 Gb Radiation Hardened Nonvolatile Memory Development

    SBC: Scientic, Inc.            Topic: X602

    The objective of this effort is to identify, characterize and develop advanced semiconductor materials and fabrication process techniques, and design and produce a Gigabit (GB)-scale high density, radiation hardened (RH), SONOS-based nonvolatile memory (NVM) in a standard, high density CMOS technology with feature sizes approaching the 90nm technology node. Highly reliable, RH SWAP-efficient, hig ...

    SBIR Phase I 2011 National Aeronautics and Space Administration
  2. 5 in 1 Drill For Mars Sample Return Mission

    SBC: Honeybee Robotics, Ltd.            Topic: S502

    NASA is investigating a Mars Sample Return Mission, consisting of at least three separate missions: 1) Mars Astrobiology Explorer-Cacher, MAX-C (sample acquisition and caching), 2) A fetch rover and the Mars Ascent Vehicle (MAV), 3) Earth Return Vehicle (ERV).The primary goal of the MAX-C mission is to acquire ~20 cores, 1cm diameter by 5cm long, and place them in a cache for return back to Earth. ...

    SBIR Phase I 2011 National Aeronautics and Space Administration
  3. A Compact Safe Cold-Start (CS2) System for Scramjets using Dilute Triethylaluminum Fuel Mixtures

    SBC: ACENT LABORATORIES LLC            Topic: A202

    This proposal leverages a highly successful Phase 1 feasibility effort to further develop a system that satisfies the cold-start requirements of scramjet engines. The system provides energy-dense, low volume hydrocarbon fuel conditioning based on the hydrolysis reaction of triethylaluminum (TEA) with water. TEA is an organometallic liquid that reacts exothermically with water and burns readily i ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
  4. A High Order Accuracy Computational Tool for Unsteady Turbulent Flows and Acoustics

    SBC: Frendi Research Corporation            Topic: A206

    The main objective of this research effort is to develop a higher order unsteady turbulent flow solver based on the FDV method, and to exploit its attributes of spanning the whole Mach number range.The well known advantages of the implicit FEM will be inherited along with robust boundary conditions implementation and sound mathematical bases. Efficient parallelization, using MPI through domain dec ...

    SBIR Phase I 2011 National Aeronautics and Space Administration
  5. A Light Weight, Mini Inertial Measurement System for Position and Attitude Estimation on Dynamic Platforms

    SBC: Impact Technologies            Topic: O405

    Impact Technologies, LLC in collaboration with the Rochester Institute of Technology, proposes to develop and demonstrate a flight-worthy hardware prototype of a miniature, low cost/weight/ power device that provides stable and highly accurate near continuous positioning, attitude, and inertial measurements while being subjected to highly dynamic maneuvers and high vibration effects. In contrast t ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
  6. A Miniaturized Sensor for Microbial Monitoring of Spacecraft Water Environment

    SBC: CFD Research Corporation            Topic: X203

    Accurate real-time microbial monitoring of water environment is of paramount importance to crew health as well as to ensure proper functioning and control of the life support system during space exploration. The existing methods are time-consuming and labor-intensive, and the devices used are bulky, consumable-hungry, and ill-suited for spacecraft deployment. We propose to develop and demonstrate ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
  7. Adaptive Aeroservoelastic Suppression for Aircraft Upset and Damage Conditions

    SBC: Impact Technologies            Topic: A107

    Impact Technologies, in collaboration with Tennessee State University, propose to develop and demonstrate an adaptive system identification and multi-loop control methodology that provides real-time aircraft structural mode suppression associated with aeroservoelastic interaction under upset and damage conditions. The proposed program will develop an effective real-time aircraft structural model, ...

    SBIR Phase I 2011 National Aeronautics and Space Administration
  8. Advanced Carbothermal Electric Reactor

    SBC: Orbital Technologies Corporation            Topic: X301

    The overall objective of the Phase 1 effort was to demonstrate the technical feasibility of the Advanced Carbothermal Electric (ACE) Reactor concept. Unlike state-of-the-art carbothermal reactors that use concentrated solar energy and/or laser energy to heat the regolith, the ACE Reactor uses an innovative method to electrically heat the regolith to temperatures over 1800ºC within a thermally ins ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
  9. Aero-Effected Distributed Adaptive Control of Flexible Aircraft Using Active Bleed

    SBC: Atair Aerospace, Inc            Topic: A207

    The proposed research focuses on the development of a new adaptive control methodology for active control of wing aerodynamic shape to effect distributed aerodynamic forces and moments for maneuvering and stabilization of flexible airframes without moving control surfaces. The new aero-effected flight control will be achieved using output feedback adaptive control of distributed bleed across aero ...

    SBIR Phase I 2011 National Aeronautics and Space Administration
  10. Aerodynamic Modeling with Heterogeneous Data Assimilation and Uncertainty Quantification

    SBC: CLEAR SCIENCE CORP            Topic: A205

    Clear Science Corp. proposes to develop an aerodynamic modeling tool that assimilates data from different sources and facilitates uncertainty quantification. The technical merit and feasibility of the technology will be demonstrated in Phase I through a series of verification and validation tests that utilize both computational and wind tunnel data in constructing aerodynamic models for the Orion ...

    SBIR Phase I 2011 National Aeronautics and Space Administration

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