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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. Sensing Aware Autonomous Communications System

    SBC: Space Micro Inc.            Topic: T501

    Space Micro and its partner research institution, the University of Arizona bring together innovations in channelization and network protocol development. Together, these innovations will provide improved hopping radios (with digital, rapidly reconfigurable implementation, wider bandwidth and reduced overhead penalty for hopping) and improved spectrum and link quality sensing. We will demonstrate ...

    STTR Phase I 2015 National Aeronautics and Space Administration
  2. Gust Load Estimation and Rejection With Application to Robust Flight Control Design for HALE Aircraft

    SBC: Systems Technology, Inc.            Topic: T401

    High Altitude Long Endurance (HALE) aircraft have garnered increased interest in recent years as they can serve several purposes, including many of the objectives of satellites while incurring a fraction of the cost to deploy. Examples applications include Intelligence, Surveillance, and Reconnaissance, communications relay systems, and environmental and atmospheric sensing. The requirements for H ...

    STTR Phase I 2015 National Aeronautics and Space Administration
  3. Innovative Aerodynamic Modeling for Aeroservoelastic Analysis and Design

    SBC: M4 ENGINEERING, INC.            Topic: T401

    We propose the development of a modern panel code for calculation of steady and unsteady aerodynamic loads needed for dynamic servoelastic (DSE) analysis of flight vehicles. The code will be especially tailored to be robust, reliable, and integrated with the NASA Object Oriented Optimization (O3) system through selection of analysis methods, file formats, and computing environment, allowing it to ...

    STTR Phase I 2015 National Aeronautics and Space Administration
  4. Improved Forecasts of Solar Particle Events using Eruptive Event Generators based on Gibson-Low and Titov-Demoulin Magnetic Configurations

    SBC: MICHIGAN AEROSPACE CORP            Topic: T602

    Radiation hazards constitute a serious risk to human and robotic space operations beyond Low-Earth orbit. Primary contributors to space radiation include Solar Particle Events (SPEs) associated with Coronal Mass Ejections (CMEs). Because the mechanisms that produce coronal mass ejections (CME) are exceedingly complex, no reliable deterministic methods for predicting eruptions are yet available, a ...

    STTR Phase I 2015 National Aeronautics and Space Administration
  5. A Coupled System for Predicting SPE Fluxes

    SBC: PREDICTIVE SCIENCE INCORPORATED            Topic: T602

    Solar Particle Events (SPEs) represent a major hazard for extravehicular maneuvers by astronauts in Earth orbit, and for eventual manned interplanetary space travel. They can also harm aircraft avionics, communication and navigation. We propose to develop a system to aid forecasters in the prediction of such events, and in the identification/lengthening of "all clear" time periods when there is a ...

    STTR Phase I 2015 National Aeronautics and Space Administration
  6. Advanced Gas Sensing Technology for Space Suits

    SBC: INTELLIGENT OPTICAL SYSTEMS, INC.            Topic: T601

    Advanced space suits require lightweight, low-power, durable sensors for monitoring critical life support materials. No current compact sensors have the tolerance for liquid water that is specifically required for portable life support systems (PLSS). Intelligent Optical Systems (IOS) will develop a luminescence-based optical sensor probe to monitor carbon dioxide, oxygen, and humidity, and select ...

    STTR Phase I 2015 National Aeronautics and Space Administration
  7. NLV Upper Stage Development and Flight Testing

    SBC: Garvey Spacecraft Corporation            Topic: T101

    The technical innovation proposed here is the design during Phase I of a high performance upper stage for a two-stage "20 / 450" Nanosat Launch Vehicle (NLV) that is configured to deliver up to 20 kg to a 450 km low Earth orbit (Figure 1). Parallel tasks prepare for the Phase II development and sub-orbital flight testing of a prototype vehicle that is directly traceable to the orbital-capable ...

    STTR Phase I 2015 National Aeronautics and Space Administration
  8. High Performance Hybrid Upper Stage for NanoLaunch Vehicles

    SBC: PARABILIS SPACE TECHNOLOGIES INC            Topic: T101

    Parabilis Space Technologies, Inc. (Parabilis), in collaboration with Utah State University (USU), proposes a low cost, high performance launch vehicle upper stage using oxygen and a novel additively manufactured polymer fuel grain as propellants in response to solicitation T1.01, Affordable Nano/Micro Launch Propulsion Stages. This technology will fulfill the ever-growing mission demands of the C ...

    STTR Phase I 2015 National Aeronautics and Space Administration
  9. Multifunctional Environmental Digital Scanning Electron Microprobe (MEDSEM)

    SBC: CHROMOLOGIC LLC            Topic: T801

    Chromologic (CL) and the California Institute of Technology (Caltech) propose to develop and demonstrate a Multifunctional Environmental Digital Scanning Electron Microprobe (MEDSEM) instrument that transmits high-energy beams of electrons sequentially from a two-dimensional array of miniaturized electron probes into a planetary atmosphere, and these electrons will strike solid or liquid planetary ...

    STTR Phase I 2015 National Aeronautics and Space Administration
  10. Fusion of Modeling and Simulation Credibility in Multidisciplinary Design

    SBC: MICHIGAN ENGINEERING SERVICES LLC            Topic: T1102

    Entry vehicle design and aircraft design are just two examples of systems that are of interest to NASA, requiring interactions and exchange of information among multiple performance disciplines. Since any computational optimization process relies on simulation models for identifying the impact of design changes in meeting performance expectations and improving metrics of goodness, it is essential ...

    STTR Phase I 2015 National Aeronautics and Space Administration
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