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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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NLV Upper Stage Development and Flight Testing
SBC: Garvey Spacecraft Corporation Topic: T101Our Phase I results include a preliminary design for an advanced nanosat launch vehicle (NLV) upper stage that features several advanced propulsion technologies, as well as extensive empirical data from a series of pathfinding operations conducted at both the Pacific Spaceport Complex - Alaska on Kodiak Island and the Poker Flat Research Range. For Phase II, we are taking major steps, such as bui ...
STTR Phase II 2017 National Aeronautics and Space Administration -
Reusable Nanocomposite Membranes for the Selective Recovery of Nutrients in Space
SBC: NANOSONIC INC. Topic: T702Through the STTR program, NanoSonic and Virginia Tech will create low-cost, reusable membranes that selectively capture and recycle nutrients (e.g., N, P, K) from urine in space. Urine is a readily available commodity in space that is rich in valuable nutrients for plant growth. Humans produce individually about 500 L of urine per year that contains ~7 g/L of nitrogen (N), ~1 g/L phosphorous (P) ...
STTR Phase I 2017 National Aeronautics and Space Administration -
Bantam Rocket Affordable SLV Stage (BRASS)
SBC: EXQUADRUM INC Topic: T101During the proposed Phase I research and development effort, the project team will integrate previously demonstrated technologies into a stage 4 propulsion system for an existing Small Launch Vehicle (SLV). The resulting fourth stage will meet launch vehicle requirements for Mass Fraction and Specific Impulse. Key stage component will be fabricated and demonstrated. The propulsion system will be ...
STTR Phase I 2017 National Aeronautics and Space Administration -
A Massively Parallel Framework for Low-Dissipation, Multiphysics Simulations of Rocket Engines
SBC: CASCADE TECHNOLOGIES INC Topic: T102In this proposal, researchers from Cascade Technologies and Stanford University outline a multi-year research plan to develop large-eddy simulation (LES) tools to predict and understand combustion instabilities in liquid-propellant rocket engines. Rocket instabilities are a notoriously complicated, multiscale problem involving nonlinear interactions between transcritical multiphase flows, turbulen ...
STTR Phase I 2017 National Aeronautics and Space Administration -
Multiphysics Framework for Prediction of Dynamic Instability in Liquid Rocket Engines
SBC: ATA ENGINEERING, INC. Topic: T102Mitigation of dynamic combustion instability is one of the most difficult engineering challenges facing NASA and industry in the development of new continuous-flow combustion systems such as the combustion chambers in liquid-fueled rocket engines (LREs). Combustion instabilities are spontaneous, self-sustaining oscillations that tie the combustor acoustics to the combustion reaction itself. These ...
STTR Phase I 2017 National Aeronautics and Space Administration -
Optical Intersatellite Communications for CubeSat Swarms
SBC: CROSS TRAC ENGINEERING, INC. Topic: T1102The growing interest in CubeSat swarm and constellation systems by NASA, the Department of Defense and commercial ventures has created a need for self-managed inter-satellite networks capable of handling large amount of data while simultaneously precisely measuring the distances between the spacecraft. CrossTrac Engineering, Inc., in cooperation with our partners Professor Kerri Cahoy of the Massa ...
STTR Phase I 2017 National Aeronautics and Space Administration -
Efficient Composite Repair Methods for Launch Vehicles
SBC: LUNA INNOVATIONS INCORPORATED Topic: T1202Polymer matrix composites are increasingly replacing traditional metallic materials in NASA launch vehicles. However, the repair and subsequent inspection methods for these materials are considerably more complicated. Typically, a composite laminate patch must be manually fabricated and bonded or co-cured to the damaged structure. To ensure high quality patches with sufficient compaction and l ...
STTR Phase I 2017 National Aeronautics and Space Administration -
Composite Repair System
SBC: GLOYER-TAYLOR LABORATORIES INC Topic: T1202GTL has developed an innovative composite repair methodology known as the Composite Repair System (CRS). In this phase I effort, CRS is being developed for the repair of damaged induced in thin-laminate composite cryotanks. In applying CRS to damaged composite structures, the required level of structural capacity is recovered to within a predetermined percentage of its original performance after ...
STTR Phase I 2017 National Aeronautics and Space Administration -
Through Wall Wireless Intelligent Sensor and Health Monitoring (TWall-ISHM) System
SBC: AMERICAN GNC CORPORATION Topic: T1301NASA's strategic needs include those related to flexible instrumentation capable of monitoring remote or inaccessible measurement locations within Stennis Space Center (SSC) testing facilities. Looking to support the advancement of NASA SSC's infrastructure, American GNC Corporation (AGNC) and the Rensselaer Polytechnic Institute (RPI) are proposing the Through Wall Wireless Intelligent Sensor and ...
STTR Phase I 2017 National Aeronautics and Space Administration -
Methodology for Distributed Electric Propulsion Aircraft Control Development with Simulation and Flight Demonstration
SBC: EMPIRICAL SYSTEMS AEROSPACE INC Topic: T1501In the proposed STTR study, Empirical Systems Aerospace, Inc. (ESAero) and the University of Illinois at Urbana-Champaign (UIUC) will create a methodology for the development of a flight control algorithm featuring differential thrust provided by a distributed electric propulsion (DEP) system. The focal piece of the study is a dynamically scaled Cirrus SR22T UAV at UIUC, which will be modified to ...
STTR Phase I 2017 National Aeronautics and Space Administration