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Award Data
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.
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Integrated Component and System Analyses of Instabilities in Test Stands
SBC: COMBUSTION RESEARCH & FLOW TECHNOLOGY INC Topic: T1001Instabilities 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 -
AggieSat: Autonomous Rendezvous and Docking Technology Demonstrator
SBC: PHYSICS, MATERIALS, AND APPLIED MATHEMATICS RESEARCH L.L.C. Topic: T601Current 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 -
Multiscale GasKinetics/Particle (MGP) Simulation for Rocket Plume/Lunar Dust Interactions
SBC: ZONA TECHNOLOGY INC Topic: T701An 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 -
High Capacity and High Voltage Composite Oxide Cathode for Li-ion Batteries
SBC: NEI CORPORATION Topic: T301Currently 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 -
Narrow Wavelength, Frequency Modulated Source at 1.5¿Wavelength
SBC: Princeton Optronics Topic: S101NASA 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 -
Extension of an Object Oriented Multidisciplinary Analysis Optimization (MDAO) Environment
SBC: ZONA TECHNOLOGY INC Topic: T201Multidisciplinary 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 -
Membrane Water Recuperator
SBC: Wolf Engineering, LLC Topic: X201One 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 -
Polarization Maintaining Coherent Fiber Bundle Array
SBC: ADVALUE PHOTONICS INC Topic: S104Future 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 -
Thermal Management System for Long-Lived Venus Landers
SBC: ADVANCED COOLING TECHNOLOGIES INC Topic: S303Long-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 -
Loop Heat Pipe with Thermal Control Valve for Passive Variable Thermal Link
SBC: ADVANCED COOLING TECHNOLOGIES INC Topic: S302Loop 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