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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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High Performance Simulation Tool for Multiphysics Propulsion Using Fidelity-Adaptive Combustion Modeling
SBC: STREAMLINE NUMERICS, INC. Topic: T102The innovation proposed here is a fidelity-adaptive combustion model (FAM) implemented into the Loci-STREAM CFD code for use at NASA for simulation of rocket combustion. This work will result in a high-fidelity, high-performance multiphysics simulation capability to enhance NASA's current simulation capability of unsteady turbulent reacting flows involving cryogenic propellants. This novel FAM m ...
STTR Phase I 2017 National Aeronautics and Space Administration -
Vision-Based Navigation for Formation Flight onboard ISS
SBC: JAYCON SYSTEMS LLC Topic: T1102The RINGS project (Resonant Inductive Near-field Generation Systems) was a DARPA-funded effort to demonstrate Electromagnetic Formation Flight and wireless power transfer in microgravity. Integration inconsistencies in both hardware and software prevented the experiment from achieving its objectives during the planned test sessions. A later project supported by NASA ARC focused on the assessment, ...
STTR Phase I 2017 National Aeronautics and Space Administration -
Maneuvering Environment for Tiltwing Aircraft with Distributed Electric Propulsion
SBC: EMBEDDED DYNAMICS LLC Topic: T1501The tiltwing class of aircraft consists of vehicles with the ability to rotate the wing and propulsion system as a unit a full 90 degrees from the standard fixed wing configuration to one in which the wing and thrust axis become perpendicular to the body axis. This thrust vectoring capability allows the aircraft to utilize thrust borne flight for vertical takeoff and landing as well as the convent ...
STTR Phase I 2017 National Aeronautics and Space Administration -
Braided Thin-Ply Tapes
SBC: OPTERUS RESEARCH AND DEVELOPMENT, INC Topic: T12Opterus proposes to develop braided thin ply composite tapes. The tapes will be braided from ultra-thin spread-tow unidirectional carbon and glass ribbons and will enable a new source and form factor for thin-ply textiles. The resulting tapes will be especially useful for thin high strain composite space deployable structures where they will allow bias plies in long parts without requiring seams. ...
STTR Phase I 2019 National Aeronautics and Space Administration -
Hybrid Anode for Electrified Aircraft Propulsion
SBC: CORNERSTONE RESEARCH GROUP INC Topic: T15Electrified Aircraft Propulsion (EAP) research is part of NASA effort to improve aircraft fuel efficiency, emissions, and noise levels. New secondary battery chemistries are required to meet the 500 ndash; 700 Wh/kg cell level specific energy needs of UAM, all-electric helicopters and regional passenger aircraft. The cycle life, currently at asymp; 1500 ndash; 3000 cycles, also needs substantial i ...
STTR Phase I 2019 National Aeronautics and Space Administration -
In-Situ Application of Multi-Layer Thermal Protection System
SBC: CORNERSTONE RESEARCH GROUP INC Topic: T12Cornerstone Research Group Inc. (CRG) proposes to advance the state-of-the-art in space vehicle Thermal Protection Systems (TPS) through in-situ application and curing of a proprietary new resin technology called MG Resin, a family of thermoset formulations. The resins are being explored with DARPA, MDA, NASA, and the Army for a range of applications including C/C hot structures, TPS, syntactic in ...
STTR Phase I 2019 National Aeronautics and Space Administration -
A Supported Liquid Membrane System for Steady State CO2 Control in a Spacecraft Cabin
SBC: REACTION SYSTEMS, INC. Topic: T6Reducing the allowable concentration of carbon dioxide (CO2) in spacecraft is a critical need for NASA. The system now used on the International Space Station (ISS) is the carbon dioxide removal assembly (CDRA). While it has performed well on the ISS, managers have concluded that using the device to reach the new ppCO2 limit of 2.0 mm Hg is not practical and a new method is needed.In this projec ...
STTR Phase I 2018 National Aeronautics and Space Administration -
Transient Acoustic Environment Prediction Tool for Launch Vehicles in Motion during Early Lift-Off
SBC: CFD RESEARCH CORPORATION Topic: T102Launch vehicles experience extreme acoustic loads dominated by rocket exhaust plume interactions with ground structures during lift-off, which can produce damaging vibro-acoustic loads on the vehicle and payloads if not properly understood and mitigated against. Existing capabilities for modeling the turbulent plume physics during early lift-off are too dissipative to accurately resolve the propag ...
STTR Phase I 2017 National Aeronautics and Space Administration -
Multi-Band Software Defined Radio Sensor System
SBC: Pegasense, LLC Topic: T13This Multiband Software Defined Radio (SDR) sensor system proposal will demonstrate the ability to operate within multiple frequency bands and across multiple technology platforms in a single transceiver. The center frequencies and bandwidths chosen are representative of current demonstrated commercial or research devices and bands used: 400 MHz, 900 MHz, and 2.4 GHz ISM bands, with bandwidths of ...
STTR Phase I 2018 National Aeronautics and Space Administration -
Particle Flow Physics Modeling for Extreme Environments
SBC: CFD RESEARCH CORPORATION Topic: T403The liberation of particles induced by rocket plume flow from spacecraft landing on unprepared regolith of the Moon, Mars, and other destinations poses high mission risks for robotic and human exploration activities. This process occurs in a combination of "extreme environments" that combine low gravity, little or no atmosphere, with rocket exhaust gas flow that is supersonic and partially rarefie ...
STTR Phase I 2013 National Aeronautics and Space Administration