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Award Data

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The Award database is continually updated throughout the year. As a result, data for FY24 is not expected to be complete until March, 2025.

Download all SBIR.gov award data either with award abstracts (290MB) or without award abstracts (65MB). A data dictionary and additional information is located on the Data Resource Page. Files are refreshed monthly.

The SBIR.gov award data files now contain the required fields to calculate award timeliness for individual awards or for an agency or branch. Additional information on calculating award timeliness is available on the Data Resource Page.

  1. Reaction Wheel with Embedded MEMS IMU

    SBC: Milli Sensor Systems and Actuators, Inc.            Topic: S405

    Reaction wheels are used to stabilize satellites and to slew their orientation from object to object with precision and accuracy by varying the rotational speed of the wheels. Three or four wheels are usually used with three of them aligned along orthogonal axes. The degree to which pointing stability is achieved depends on the stability of the wheels' angular momentum vectors while spinning, ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
  2. GPU-Accelerated Sparse Matrix Solvers for Large-Scale Simulations

    SBC: EM PHOTONICS INC            Topic: S601

    At the heart of scientific computing and numerical analysis are linear algebra solvers. In scientific computing, the focus is on the partial differential equations (PDEs) that arise from computational fluid dynamics (CFD), climate modeling, astrophysics, and structural and heat analysis that cannot be solved analytically. Certain problem formulations lead to sparse matrices, in which the majority ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
  3. Robotic Vehicle Proxy Simulation

    SBC: Energid Technologies Corporation            Topic: X101

    Energid Technologies proposes the development of a digital simulation to replace robotic vehicles in field studies. It will model the dynamics, terrain interaction, sensors, control, communications, and interfaces of a robotic vehicle with the goal of supporting validation and training. The simulation will be very easy to use by simple execution on a networked PC. It will connect to NASA's ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
  4. Fast Neutron Dosimeter for the Space Environment

    SBC: RADIATION MONITORING DEVICES, INC.            Topic: X1401

    Model calculations and risk assessment estimates indicate that secondary neutrons, with energies ranging between 0.5 to>150 MeV, make a significant contribution to the total absorbed dose received by space crews during long duration space missions [1-3]. Advanced scintillation materials, which exhibit radiation type and mass dependent emission times, coupled to SSPM detectors, provide the optimum ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
  5. Reconfigurable VLIW Processor for Software Defined Radio

    SBC: ARIES DESIGN AUTOMATION, LLC            Topic: O103

    We will implement an environment for design, formal verification, compilation of code, and performance and power evaluation of Systems on a Chip (SOCs) consisting of heterogeneous processor cores that can be single-issue pipelined, superscalar, or VLIW, and are binary-code compatible with any existing Instruction Set Architecture (ISA). Particularly, we will ensure binary-code compatibility with t ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
  6. Magnesium Based Rockets for Martian Exploration

    SBC: BUSEK CO., INC.            Topic: S308

    In the proposed Phase II program, we will continue the development of Mg bipropellant rockets for Martian PAV applications. In Phase I, we proved the feasibility of this game-changing technology. Through chemical analysis, we determined that Mg can be combusted with CO2 condensed in-situ from the Martian atmosphere to yield Isp ~240 s. We then successfully demonstrated a low fidelity Mg-CO2 roc ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
  7. In-Flight and Pre-Flight Detection of Pitot Tube Anomalies

    SBC: ANALYSIS AND MEASUREMENT SERVICE CORPORATION            Topic: A110

    The health and integrity of aircraft sensors play a critical role in aviation safety. Unfortunately, inaccurate or false readings from these sensors can lead to improper decision-making resulting in serious and sometimes fatal consequences. The research performed in Phase I demonstrated the feasibility of using advanced data analysis techniques to identify anomalies in Pitot tubes resulting from ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
  8. Advanced Bayesian Methods for Lunar Surface Navigation

    SBC: Autonomous Exploration, Inc.            Topic: O403

    The key innovation of this project is the application of advanced Bayesian methods to integrate real-time dense stereo vision and high-speed optical flow with an Inertial Measurement Unit (IMU) to produce a highly accurate planetary rover navigation system. The software developed in this project leverages current computing technology to implement advanced Visual Odometry (VO) methods that will acc ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
  9. High Radiation Resistance Inverted Metamorphic Solar Cell

    SBC: MICROLINK DEVICES INC            Topic: S303

    The innovation in this SBIR Phase II project is the development of a unique triple junction inverted metamorphic technology (IMM), which will enable the manufacturing of very lightweight, low-cost, InGaAsP-based multijunction solar cells. The proposed IMM technology is based on ELO (epitaxial lift-off) and consists of Indium (In) and Phosphorous (P) solar cell active materials, which are designed ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
  10. Low Mass Low Power Hall Thruster System

    SBC: BUSEK CO., INC.            Topic: S304

    In NASA is seeking an electric propulsion system capable of producing 20mN thrust with input power up to 1000W and specific impulse ranging from 1600-3500 seconds. The key technical challenge of the topic is the target mass of 1kg for the thruster and 2kg for the power processor (PPU). In Phase 1 Busek develop an overall subsystem design for the thruster/cathode, PPU and XFS. The feasibility of ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
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