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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. Integrated Component and System Analyses of Instabilities in Test Stands

    SBC: COMBUSTION RESEARCH & FLOW TECHNOLOGY INC            Topic: T1001

    Instabilities associated with the operation of liquid rocket propulsion systems and test facilities usually manifest themselves as structural vibrations and may cause structural damage. While the source of the instability is directly related to the performance of a component such as a turbopump, the associated pressure fluctuations as they propagate through the system have the potential to amplify ...

    STTR Phase II 2010 National Aeronautics and Space Administration
  2. AggieSat: Autonomous Rendezvous and Docking Technology Demonstrator

    SBC: PHYSICS, MATERIALS, AND APPLIED MATHEMATICS RESEARCH L.L.C.            Topic: T601

    Current autonomous rendezvous and docking (AR&D) capability in low Earth orbit (LEO) is constrained by sensor and effector mass, power, and accuracy limits. To this end, NASA Johnson Space Center has developed a GPS receiver, called DRAGON (Dual RF Astrodynamic GPS Orbital Navigator), specifically to address the sensor constraints. The proposed innovation includes creating a small, low-cost, and v ...

    STTR Phase II 2010 National Aeronautics and Space Administration
  3. Multiscale GasKinetics/Particle (MGP) Simulation for Rocket Plume/Lunar Dust Interactions

    SBC: ZONA TECHNOLOGY INC            Topic: T701

    An efficient and accurate software package named ZMGP (ZONA Multi-scale Gaskinetic/Particle simulation package) is proposed as a 3D tool to predict the lunar dust trajectory and crater formation process when a retro-rocket lands on the lunar surface. ZMGP has many special features including: 1, the hybrid flow module by coupling the gaskinetic Bhatnagar-Gross-Krook (BGK) model and the direct simul ...

    STTR Phase II 2010 National Aeronautics and Space Administration
  4. High Capacity and High Voltage Composite Oxide Cathode for Li-ion Batteries

    SBC: NEI CORPORATION            Topic: T301

    Currently used cathode materials in energy storage devices do not fully satisfy the power density and energy density requirements for NASA's exploration missions. Working in collaboration with our STTR partner at University of California – San Diego, we propose to develop layered-layered composite cathode materials that offer superior performance over commercially available positive electrode mat ...

    STTR Phase II 2010 National Aeronautics and Space Administration
  5. Narrow Wavelength, Frequency Modulated Source at 1.5¿Wavelength

    SBC: Princeton Optronics            Topic: S101

    NASA needs narrow linewidth lasers in the 1.5 or 2 micron wavelength regime for Lidar applications. The laser should be tunable by several nm and frequency modulated by 5GHz. Princeton Optronics has developed ultra-stable narrow linewidth diode pumped solid state lasers and developed high power Vertical Cavity Surface Emitting Laser (VCSEL) devices for fiber laser pumps as well as VCSEL pumped CW ...

    SBIR Phase I 2010 National Aeronautics and Space Administration
  6. Extension of an Object Oriented Multidisciplinary Analysis Optimization (MDAO) Environment

    SBC: ZONA TECHNOLOGY INC            Topic: T201

    Multidisciplinary design, analysis, and optimization (MDAO) tools today possess limited disciplines with little fidelity modeling capability. These tools are typically developed as a single large software application that performs analysis for all disciplines but has little or no capability to integrate multi-fidelity and multi-discipline components that have already been developed as stand-alone ...

    STTR Phase I 2010 National Aeronautics and Space Administration
  7. Membrane Water Recuperator

    SBC: Wolf Engineering, LLC            Topic: X201

    One of the CO2 reduction technologies currently being developed by NASA is the CO2 and Moisture Removal Amine Swing-bed System (CAMRAS). One of the disadvantages of the CAMRAS for long duration missions is that it removes moisture in addition to CO2. One way to minimize the water loss from the atmosphere, yet still be able to implement the highly desirable CO2 removal function of the CAMRAS, is to ...

    SBIR Phase I 2010 National Aeronautics and Space Administration
  8. Polarization Maintaining Coherent Fiber Bundle Array

    SBC: ADVALUE PHOTONICS INC            Topic: S104

    Future NASA flight missions are considering passive wavefront and amplitude control in astronomical applications such as the search for exo-planets. NASA's Discovery mission proposal called out the need for a coherent 2-dimensional array of fiber bundles for this application. In this SBIR proposal we propose to develop monolithic polarization maintaining (PM) coherent fiber bundle arrays consistin ...

    SBIR Phase I 2010 National Aeronautics and Space Administration
  9. Thermal Management System for Long-Lived Venus Landers

    SBC: ADVANCED COOLING TECHNOLOGIES INC            Topic: S303

    Long-lived Venus landers require power and cooling. Heat from the roughly 64 General Purpose Heat Source (GPHS) modules must be delivered to the convertor with minimal ÄT. The cooling system must be shutoff during the transit to Venus without overheating the GPHS modules. This program will develop an alkali metal Variable Conductance Heat Pipe (VCHP) integrated with a two-phase heat collection/tr ...

    SBIR Phase I 2010 National Aeronautics and Space Administration
  10. Loop Heat Pipe with Thermal Control Valve for Passive Variable Thermal Link

    SBC: ADVANCED COOLING TECHNOLOGIES INC            Topic: S302

    Loop heat pipes (LHPs) can provide variable thermal conductance needed to maintain electronics and batteries on Lunar/Martian rovers/landers within desired temperature range. During lunar day, the LHP transfers the heat to the radiator for rejection. During the fourteen-day-long lunar night, the sink temperature drops, lowering LHP and WEB/battery temperatures. Without a variable thermal link, the ...

    SBIR Phase I 2010 National Aeronautics and Space Administration
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