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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. A UAS-ATC Simulation Test-Bed

    SBC: Sandia Research Corporation            Topic: A501

    The proposed solution is to create a high fidelity simulation environment that merges a UAS ground control station (GCS) simulator with an air traffic control (ATC) simulator. The UAS GCS station will have the capability of introducing a single UAS or multiple UASs simulator operated by a single and/or multiple UAS pilots into the ATC. This simulation will have the ability to simulate manned aircr ...

    SBIR Phase I 2012 National Aeronautics and Space Administration
  2. Load-Bearing Inflatables Using Light-Curing Rigidization Technology

    SBC: Adherent Technologies, Inc.            Topic: X501

    NASA is soliciting new concepts for lightweight stabilized inflatables in regards to low weight, high storage density, and ease of deployment. What most of the inflatable concepts are lacking is the ability for integrated structural members that do not require permanent inflation pressure. Any structure requiring inflation pressure for structural stability becomes hazardous in case of puncture d ...

    SBIR Phase I 2012 National Aeronautics and Space Administration
  3. Very large computer generated holograms for precision metrology of aspheric optical surfaces

    SBC: Arizona Optical Metrology LLC            Topic: S205

    Both ground and space telescopes employ aspheric mirrors. A particular example is the X-ray telescope where primary and secondary mirrors have nearly cylindrical surfaces. Computer Generated Holograms (CGH), in combination with commercial interferometers, provide high resolution and high accuracy measurements of aspheric optical surfaces. The current state of the art CGHs are made on 6" square sub ...

    SBIR Phase I 2012 National Aeronautics and Space Administration
  4. Braided Composite Technologies for Rotorcraft Structures

    SBC: A & P TECHNOLOGY, INC.            Topic: A209

    The proposed program will focus on the development of a new generation of advanced technology for rotorcraft transmission systems. This program will evaluate the viability of integrating gears with composite shafts. The aim of this work is to reduce overall weight and improve vibration characteristics. Two concepts have been identified and will be further researched. The first design includes c ...

    SBIR Phase I 2012 National Aeronautics and Space Administration
  5. Predictive Gust Load Alleviation Control Using Leading Edge Stagnation Point Sensor

    SBC: ZONA TECHNOLOGY INC            Topic: A207

    ZONA Technology, Inc. proposes an R & D effort to develop a Gust Load Alleviation (GLA) control system using a novel Leading Edge Stagnation Point (LESP) sensor that has the nearly instantaneous predictive capability. The real-time gust information from the sensor will enhance the performance of the proposed GLA control system. The GLA control method we will adopt is the Generalized Predictive Con ...

    SBIR Phase I 2012 National Aeronautics and Space Administration
  6. Fast Responding Pressure-Sensitive Paint for Large-Scale Wind Tunnel Testing

    SBC: INNOVATIVE SCIENTIFIC SOLUTIONS INC            Topic: A209

    The proposed work focuses on implementing fast-response pressure-sensitive paint for measurements of unsteady pressure in rotorcraft applications. Significant rotorcraft problems such as dynamic stall, rotor blade loads in forward flight, and blade-vortex interaction all have significant unsteady pressure oscillations that must be resolved in order to understand the underlying physics. Installatio ...

    SBIR Phase I 2012 National Aeronautics and Space Administration
  7. Tunable Interior Rotorcraft Noise Control

    SBC: CORNERSTONE RESEARCH GROUP INC            Topic: A209

    CRG has recently developed a new class of shape memory polymers (SMP) that are electrically activated, as opposed to the more mature thermally activated SMPs. Electrically activated shape memory polymers (EASMP) open a new design space of unexplored functionality beyond what has been considered for thermally activated materials. This project will combine the advantages of EASMP with the design of ...

    SBIR Phase I 2012 National Aeronautics and Space Administration
  8. Fast Flow Cavity Enhanced Ozone Monitor

    SBC: SOUTHWEST SCIENCES INC            Topic: S108

    Naturally occurring in the stratosphere, ozone plays a significant role in many atmospheric reactions, cloud formation, and is the key player in shielding harmful UV radiation. In the troposphere, it is a criteria pollutant produced via photochemical smog reactions, and is key in the formation of organic aerosols from VOCs. A better understanding on the distribution of ozone and its influences o ...

    SBIR Phase I 2012 National Aeronautics and Space Administration
  9. Skin Friction and Pressure Measurements in Supersonic Inlets

    SBC: INNOVATIVE SCIENTIFIC SOLUTIONS INC            Topic: A210

    Supersonic propulsion systems include internal ducts, and therefore, the flow often includes shock waves, shear layers, vortices, and separated flows. Passive flow control devices such as micro-vortex generators and micro-ramps have been proposed to improve vehicle performance. The ability to measure surface quantities such as skin friction and unsteady pressure on the inlet model would provide in ...

    SBIR Phase I 2012 National Aeronautics and Space Administration
  10. Simultaneous Skin Friction and Pressure Sensitive Paint

    SBC: INNOVATIVE SCIENTIFIC SOLUTIONS INC            Topic: A401

    Currently, the contribution of skin friction to the total drag of a wind tunnel model is estimated by comparing measurements of the total drag to the integrated pressure drag. While this yields an estimate for the average skin friction, the distribution of the skin friction cannot be determined from such measurements. The distribution of skin friction and pressure is available from computational f ...

    SBIR Phase I 2012 National Aeronautics and Space Administration
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