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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. 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
  2. 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
  3. Acousto-Optic Tunable Filter-Based Polarimetric Spectral Sensor With Progressive Algorithm For Material Analysis and Mapping

    SBC: BRIMROSE TECHNOLOGY CORP            Topic: T801

    One of the strategic goals of NASA's Planetary Science Mission is to advance scientific knowledge of the origin and history of the solar system, the potential for life elsewhere. The current STTR addresses this strategic goal. The proto-type AOTF-based SWIR spectropolarimetric imaging system developed in Phase I (which will be further optimized and integrated with optimal algorithm/software in Pha ...

    STTR Phase II 2015 National Aeronautics and Space Administration
  4. Advanced Design Tools for Electrosail Propulsion Systems

    SBC: PARTICLE MATTERS, INC            Topic: T2

    The goal of this project is to develop a medium-fidelity, engineering level computational tool that will provide NASA researchers with an efficient instrument for testing, optimizing, and finalizing the E-Sail configuration, and further assist in the navigation and control design. The core of the tool is a computationally efficient parallel 3Dnbsp;Particle-In-Cell (PIC)nbsp;code. The relatively sl ...

    STTR Phase I 2020 National Aeronautics and Space Administration
  5. 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
  6. 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
  7. An End-To-End Microfluidic Platform for Engineering Life Supporting Microbes in Space Exploration Missions

    SBC: HJ SCIENCE & TECHNOLOGY INC            Topic: T601

    HJ Science & Technology (HJS&T) and Lawrence Berkeley National Laboratory (LBNL) propose a highly integrated, programmable, and miniaturized microfluidic automation platform capable of running rapid and complex synthetic biology and bioengineering processes for engineering life supporting microbes in space exploration missions. Our approach combines the microfluidic automation technology of HJS&T ...

    STTR Phase II 2015 National Aeronautics and Space Administration
  8. A New Oxygen Recovery Process to Reduce Waste from Propellant Tanks

    SBC: TDA RESEARCH, INC.            Topic: T2

    After landing, the lunar lander liquid oxygen tank may contain as much as 5% residual oxygen that is pressurized with helium. TDA Research proposes to develop an oxygen recovery module which separates the helium from the oxygen so that the remaining high purity oxygen can be readily supplied to life-support equipment and fuel cells. The oxygen recovery module uses an advanced sorbent that has a hi ...

    STTR Phase I 2020 National Aeronautics and Space Administration
  9. A Robust Architecture for Sampling Small Bodies

    SBC: ADVANCED SPACE LLC            Topic: T402

    This proposal will develop an innovative architecture and concept of operations that permits reliable, safe, and repeated sampling of small bodies. The Lofted Regolith Sampling (LoRS) architecture is based on advanced astrodynamics and autonomy that is robust to target-body uncertainties and is adaptive during operations. The LoRS architecture is based on several key phases that ultimately lead to ...

    STTR Phase I 2015 National Aeronautics and Space Administration
  10. A Scalable Gas-Particle Flow Simulation Tool for Lander Plume-Surface Interaction and Debris Prediction

    SBC: CFD RESEARCH CORPORATION            Topic: T9

    Plume-regolith interaction during propulsive landing results in (1) the liberation of dust/debris particles that may collide and strike the landing vehicle and surrounding assets obscuring ground observation for safe landing and (2) craters that are formed on the landing surface, posing additional challenges to vehicle stability and surface operations. The Gas-Granular Flow Solver (GGFS) had previ ...

    STTR Phase II 2020 National Aeronautics and Space Administration
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