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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. Accommodation integrated technology to minimize the impact of disability on students' assessment

    SBC: 3-C Institute for Social Development, Inc.            Topic: N/A

    There is growing interest in computerized systems to increase accessibility of assessments for students with disabilities. Technology offers an ideal platform for implementing Universal Design (UD) principles for assessment to better accommodate student diversity and support broad student participation. The goal of this Phase II SBIR project is to continue the research and development of Assess2Pr ...

    SBIR Phase II 2014 Department of Education
  2. Commercializing the Effective K-3 Assessment to Instruction (A2i) Intervention to Reduce Cost and to Scale Access to the Benefit of More Students

    SBC: Learning Ovations, Inc.            Topic: N/A

    Purpose: Students who fail to achieve proficient levels of literacy are at increased risk for grade retention, referral to special education, and dropping out of high school. The kindergarten through 3rd grade years are particularly important for students to gain a strong foundation in reading as those who continue to struggle with reading are significantly less likely to achieve reading proficien ...

    SBIR Phase II 2014 Department of Education
  3. Atmospheric Lidar with Cross-Track Scanning

    SBC: LITESPAR INC            Topic: E301

    An eye-safe, multispectral cross-track scan subsystem with a large receiver aperture and a narrow FOV is proposed for the NASA Cloud Physics Lidar (CPL) to increase the horizontal scan area coverage. The /-14 degree cross-track scan capability will cover /- 5 km from nadir at a 20 km altitude. The cross-track scanner uses a bidirectional scan pattern, which collects 10,000 data points per cross ...

    SBIR Phase II 2014 National Aeronautics and Space Administration
  4. Highly Efficient Solid Oxide Electrolyzer & Sabatier System

    SBC: PARAGON SPACE DEVELOPMENT CORPORATION            Topic: H101

    Paragon Space Development Corporation (Paragon) and ENrG Incorporated (ENrG) are teaming to provide a highly efficient reactor for carbon monoxide/carbon dioxide (CO/CO2) conversion into methane (CH4). The system is a gravity-independent, compact, leak-tight, Solid Oxide Electrolyzer (SOE) system with embedded Sabatier reactors (ESR). Applying Corning Incorporated (Corning) Intellectual Property ( ...

    SBIR Phase II 2014 National Aeronautics and Space Administration
  5. Energy-Deposition to Reduce Skin Friction in Supersonic Applications

    SBC: PHYSICS, MATERIALS, AND APPLIED MATHEMATICS RESEARCH L.L.C.            Topic: A304

    NASA has drawn attention to an impending need to improve energy-efficiency in low supersonic (M

    SBIR Phase II 2014 National Aeronautics and Space Administration
  6. A Real-Time Fault Management Software System for Distributed Environments

    SBC: INTERNATIONAL ASSOCIATION OF VIRTUAL ORGANIZATIONS, INCORPORATED            Topic: S505

    Fault Management (FM) is critical to mission operations and particularly so for complex instruments – such as those used for aircraft and spacecraft. FM software and methodologies, however, too often have nagging limitations that restrict utility, and research and development continues to grapple relative to advancements in the complex systems they monitor. Modern spacecraft, for example, may hav ...

    SBIR Phase II 2014 National Aeronautics and Space Administration
  7. Navsonde Atmospheric Sampler

    SBC: L3 Latitude, LLC            Topic: S305

    The proposed innovation is a low-cost, retrievable and reusable, autonomously guided dropsonde capable of deploying from a host aircraft and performing in-situ atmospheric measurements. We have decided to name this platform the NavSonde−an autonomously navigable sonde-glider. The proposed effort focuses on the engineering work involved with the retrieval of high altitude volcanic ash plume samp ...

    SBIR Phase II 2014 National Aeronautics and Space Administration
  8. Ultra High Temperature Refractory Materials

    SBC: ADVANCED CERAMICS MANUFACTURING, LLC            Topic: T1001

    Legacy refractory materials that have origins dating to the original Saturn program are commonly used in current launch facilities. Although they fail to meet the target requirements, they are the only approved material. Our research team has demonstrated a baseline system during the Phase I effort that combines a non-cement binder, a high temperature macro aggregate, and reactive nano aggregates ...

    STTR Phase II 2014 National Aeronautics and Space Administration
  9. Innovative Structural and Material Concepts for Low-Weight Low-Drag Aircraft Design

    SBC: ZONA TECHNOLOGY INC            Topic: A301

    The overall technical objective of this multi-phase project is to develop and validate a so-called 'AAW-Process' that consists of (i) the Active Aeroelastic Wing (AAW) technology of employing multiple control surfaces in tandem for achieving loads alleviation and drag minimization using the over-determined trim capability of ZONA Euler Unsteady Solver (ZEUS), and (ii) the aeroelastic tailoring tec ...

    SBIR Phase II 2014 National Aeronautics and Space Administration
  10. Six-Axis Force-Torque Transducer for Mars 2018 Mission

    SBC: ATI Industrial Automation, Inc.            Topic: S502

    A transducer element that is hearty enough for a Mars lander mission needs to be developed so that a six-axis force and torque transducer is possible. The technical objectives are: 1. A transducer element capable of surviving temperatures from -135?C to +125?C. 2. The transducer element in objective 1 with temperature compensation to minimize span and offset drift from -80?C to +70?C. 3. The tran ...

    SBIR Phase II 2014 National Aeronautics and Space Administration
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