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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. 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
  3. 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
  4. High Efficiency, High Output Plastic Melt Waste Compactor (HEHO-PMWC)

    SBC: Orbital Technologies Corporation            Topic: X202

    The innovative High Efficiency, High Output Plastic Melt Waste Compactor (HEHO-PMWC) is a trash dewatering and volume reduction system that uses heat melt compaction to remove nearly 100% of water from trash and reduce the volume by up to 11 times. The HEHO-PMWC system incorporates novel methods to compress the trash, recover water, and remove the resultant plastic tiles. This system requires acce ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
  5. 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
  6. 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
  7. 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
  8. High Efficiency Hall Thruster Discharge Power Converter

    SBC: BUSEK CO., INC.            Topic: S304

    Busek leveraged previous, internally sponsored, high power, Hall thruster discharge converter development which allowed it to design, build, and test new printed circuit board converter within this Phase 1 effort. The new converter consists of two series or parallel boards (slices) intended to power NASA GRC HiVHAC thruster or other similarly sized EP devices. The converter accepts 80 to 160V in ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
  9. Hot Gas TVC For Planetary Ascent Vehicle

    SBC: TOTALLY BENIGN ENTERPRISES INC            Topic: S308

    A Mars ascent vehicle (MAV) uses solid rocket motors to propel soil samples into orbit, but the motors cannot provide steering. Flexseal TVC control is planned for the first stage while hydrazine thrusters will be used for spin stabilization of the second stage. This approach is heavy and results in a spinning sample container in orbit, which is difficult to recover. Wickman Spacecraft & Propulsi ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
  10. Non-Toxic Ionic Liquid Fuels for Exploration Applications

    SBC: Orbital Technologies Corporation            Topic: X1001

    ORBITEC proposes to develop and test new, non-toxic ionic liquid fuels for propulsion applications. Vintage propulsion systems frequently use highly toxic propellants such as MMH. The toxicity of these propellants increases not only the risk of the missions but also the expense, due to special handling required during the entire lifetime of the propellant. Replacing toxic propellants with stron ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
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