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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. Flight Adaptive Blade for Optimum Rotor Response (FABFORR)

    SBC: CONTINUUM DYNAMICS INC            Topic: A209

    While past research has demonstrated the utility and benefits to be gained with the application of advanced rotor system control concepts, none have been implemented to date on a production military or commercial rotorcraft. A key contributor to this fact is the inherent cost associated with installation and maintenance of these control systems, since many system designs require the replacement o ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
  2. Design Environment for Multi-Fidelity and Multi-Disciplinary Components

    SBC: MECHANICAL SOLUTIONS INC            Topic: A208

    Many of the most challenging categories of propulsion system development are related to the prediction of interacting effects between the fluid loads, thermal loads, and the structural deflection. In practice, the interactions between technical disciplines are often not fully explored analytically, and the analysis in one discipline often uses a simplified representation of other disciplines as an ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
  3. Blade Vibration Measurement System for Unducted Fans

    SBC: MECHANICAL SOLUTIONS INC            Topic: A401

    With propulsion research programs focused on new levels of efficiency and noise, there are two emerging avenues for advanced gas turbine technology: the geared turbofan and ultra-high bypass ratio fan engines. Both of these candidates are being pursued as collaborative research projects between NASA and the engine OEMs. The high bypass concept from GE Aviation is an unducted fan which features a b ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
  4. Fault Tolerant Software-Defined Radio on Manycore

    SBC: MAXENTRIC TECHNOLOGIES LLC            Topic: O103

    Mobile communications systems require programmable embedded platforms that can handle computationally demanding signal processing codes without the burden of high power consumption. As hardware performance improves, technology trends have shifted functionality from the gate level up to software, as demonstrated by the emergence of software defined radio. Traditionally, these platforms rely on FPGA ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
  5. Low-Noise, UV-to-SWIR Broadband Photodiodes for Large-Format Focal Plane Array Sensors

    SBC: DISCOVERY SEMICONDUCTORS, INC.            Topic: S105

    Broadband focal plane arrays, operating in UV-to-SWIR wavelength range, are required for atmospheric monitoring of greenhouse gases. Currently, separate image sensors are used for different spectral sub-bands: GaN for UV, Si for visible, and InGaAs for SWIR, requiring expensive component-level integration for hyper-spectral imaging. Also, the size of the InGaAs focal plane arrays is currently limi ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
  6. NFAD Arrays for Single Photon Optical Communications at 1.5 um

    SBC: Princeton Lightwave, Inc.            Topic: O106

    For this program, we propose to develop large pixel-count single photon counting detector arrays suitable for deployment in spacecraft terminal receivers supporting long-range laser communication systems at 1.5 um. To surmount the present obstacles to higher photon counting rate -- as well as the complexity of back-end circuitry required -- in using conventional single photon avalanche diodes (SPA ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
  7. Narrow Wavelength, Frequency Modulated Source at 1.5 Wavelength

    SBC: Princeton Optronics            Topic: S101

    Ultrastable, narrow linewidth, tunable, high reliability sources at 1.5 or 2mm are needed for high performance LIDARs for several NASA applications, including wind speed measurement, surface topography, earth and planetary atmosphere composition measurements. Princeton Optronics proposes to develop a low noise, narrow linewidth, 10W output MOPA source at 1500nm using a tunable, low noise, narrow l ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
  8. Expandable/Foldable Structures for Habitat

    SBC: FOLDED STRUCTURES COMPANY LLC            Topic: X402

    Folded Structures Company (FSC) has developed an innovative design approach for multi-laminate, primary and secondary structures for planetary habitats that integrates the dynamic deployment means with the static structural design using an advanced mathematical folding theory. The design approach holds the promise of a much simpler expandable structure that is both lightweight and compactable (lo ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
  9. Extended Wavelength InP Based Avalanche Diodes for MWIR Response

    SBC: Princeton Lightwave, Inc.            Topic: T501

    For this NASA STTR program, we propose to develop a novel superlattice-based near infrared to midwave infrared avalanche photodetector (APD) grown on InP substrates for single photon counting applications at high operating temperatures on the order of 200K accessible using thermoelectric coolers. This enables a detector with broad spectral response spanning 0.9 to 4 & #956;m wavelength with reduce ...

    STTR Phase I 2011 National Aeronautics and Space Administration
  10. Extremely High Suction Performance Inducers for Space Propulsion

    SBC: Concepts NREC, LLC            Topic: T901

    The proposed innovation provides a way to design low flow coefficient inducers that have higher cavitation breakdown margin, larger blade angles, thicker more structurally robust blades, and better off-design flow stability than the current state-of-the-art designs. The technology will increase the structural, stability, and suction margin of inducers designed in the currently acceptable flow coe ...

    STTR Phase II 2011 National Aeronautics and Space Administration
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