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The Award database is continually updated throughout the year. As a result, data for FY23 is not expected to be complete until September, 2024.

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. Compact Raman Air Sensor

    SBC: MESA PHOTONICS LLC            Topic: T601

    Mesa Photonics, in collaboration with the College of Optics and Photonics (CREOL) at the University of Central Florida, proposes to develop a spacesuit gas sensor based upon its Enhanced Raman Gas Sensor (ERGS) technology. The goal a moisture tolerant, drop-in replacement for the current CO2 sensor. Preliminary work achieved detection sensitivities for CO2, CH4, O2, and N2 of 1000, 300, 1000 and 1 ...

    STTR Phase I 2015 National Aeronautics and Space Administration
  2. Spacesuit Multigas Monitor

    SBC: SOUTHWEST SCIENCES INC            Topic: T601

    Southwest Sciences Inc. (SWS), in collaboration with the Southwest Research Institute (SwRI), will develop a reliable, ultra compact, low power diode laser multigas sensor to measure carbon dioxide (CO2), ammonia (NH3), oxygen (O2) and water vapor (H2O) concentrations in the presence of saturated and condensable water concentrations appropriate for NASA's portable life support system (PLSS). A hig ...

    STTR Phase I 2015 National Aeronautics and Space Administration
  3. ACE Booster

    SBC: GLOYER-TAYLOR LABORATORIES INC            Topic: T102

    GTL has been developing a suite of transformational technologies that have the capability to disrupt the traditional launch vehicle paradigm. BHL composite cryotank technology provides a four times improvement over large aluminum iso-grid tanks, offering a 6 percentage point improvement in small stage PMF. Superior Stability Engine is an innovative liquid rocket engine configured to maximize comb ...

    STTR Phase II 2015 National Aeronautics and Space Administration
  4. Free-Flying Unmanned Robotic Spacecraft for Asteroid Resource Prospecting and Characterization

    SBC: Honeybee Robotics, Ltd.            Topic: T402

    In Phase 2 we will develop a fully integrated, autonomous free-flying robotic system based on a commercial SkyJib quadcopter, and demonstrate flying straight and level to a target location, acquisition of rock and regolith samples, and return to the point of origin. The work plan for Phase 2 is as follows: 1. Completion of the Guidance, Navigation, Control, Vision, and Sample Acquisition subsyste ...

    STTR Phase II 2015 National Aeronautics and Space Administration
  5. The World is Not Enough (WINE): Harvesting Local Resources for Eternal Exploration of Space

    SBC: Honeybee Robotics, Ltd.            Topic: T402

    The paradigm of exploration is changing. Smaller, smarter, and more efficient systems are being developed that could do as well as large, expensive, and heavy systems in the past. The 'science' fiction becomes reality fueled by advances in computing, materials, and nano-technology. These new technologies found their way into CubeSats – a booming business in the 21st century. CubeSats are no l ...

    STTR Phase I 2015 National Aeronautics and Space Administration
  6. Improved Models for Prediction of Locally Intense Aeroacoustic Loads and Vibration Environments

    SBC: ATA ENGINEERING, INC.            Topic: T1201

    ATA Engineering, Inc. proposes an STTR program to develop innovative tools and methods that will significantly improve the accuracy of random vibration response predictions for aerospace structures under critical inhomogeneous aeroacoustic loads. This will allow more accurate predictions of structural responses to be made, potentially reducing vehicle weight and cost and improving the reliability ...

    STTR Phase II 2015 National Aeronautics and Space Administration
  7. Multiple High-Fidelity Modeling Tools for Metal Additive Manufacturing Process Development

    SBC: CFD RESEARCH CORPORATION            Topic: T1204

    Despite the rapid commercialization of additive manufacturing technology such as selective laser melting, SLM, there are gaps in process modeling and material property prediction that contribute to slow and costly process development, process qualification and product certification. To address these gaps, CFDRC and our partner Dr. Kevin Chou, University of Alabama, will develop multiple computatio ...

    STTR Phase II 2015 National Aeronautics and Space Administration
  8. 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
  9. Advanced Hybrid Stage

    SBC: GLOYER-TAYLOR LABORATORIES INC            Topic: T101

    The proposed technology builds off GTL's advanced solid ramjet fuel. The method uses additive manufacturing methods to produce an innovative new type of fuel grain that regresses quickly and has a high Isp and combustion efficiency. With this technology, the performance of a liquid rocket engine can be had with a hybrid rocket system. This technology allows for a simple, low cost, high performanc ...

    STTR Phase I 2015 National Aeronautics and Space Administration
  10. 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
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